diff --git a/.gitignore b/.gitignore index 4f37a05a..162ad91f 100644 --- a/.gitignore +++ b/.gitignore @@ -34,3 +34,5 @@ examples/lookup-based_wake_steering_florisstandin/inputs/amr_standin_data.csv # Documentation build docs/_build/ +# FAST.Farm output files +*.out diff --git a/examples/FAST.Farm_interface/FF_runscript.py b/examples/FAST.Farm_interface/FF_runscript.py new file mode 100644 index 00000000..7bb3311b --- /dev/null +++ b/examples/FAST.Farm_interface/FF_runscript.py @@ -0,0 +1,29 @@ +import os + +import pandas as pd +from hercules.utilities import load_yaml +from hycon.controllers import LookupBasedWakeSteeringController +from hycon.design_tools.wake_steering_design import compute_hysteresis_zones +from hycon.interfaces.rosco_zmq_interface import ROSCO_Emulator, ROSCO_ZMQInterface + +input_dict = load_yaml(os.path.join("inputs", "hercules_input.yaml")) + +use_hysteresis = False + +# Load the optimal yaw angle lookup table for controller use. +df_opt = pd.read_pickle(os.path.join("inputs", "yaw_offsets.pkl")) + +# Optionally, add hysteresis +if use_hysteresis: + hysteresis_dict = compute_hysteresis_zones(df_opt, min_zone_width=8.0, verbose=True) +else: + hysteresis_dict = None + +interface = ROSCO_ZMQInterface(input_dict) +controller = LookupBasedWakeSteeringController( + interface, input_dict, df_yaw=df_opt, hysteresis_dict=hysteresis_dict, verbose=True +) +# interface.addcontroller(controller) + +emulator = ROSCO_Emulator(interface, controller) +emulator.startserverandsim() diff --git a/examples/FAST.Farm_interface/construct_yaw_offsets.py b/examples/FAST.Farm_interface/construct_yaw_offsets.py new file mode 100644 index 00000000..7e4d077b --- /dev/null +++ b/examples/FAST.Farm_interface/construct_yaw_offsets.py @@ -0,0 +1,57 @@ +import argparse +import os + +import numpy as np +import pandas as pd +import yaml +from floris import FlorisModel +from hycon.design_tools.wake_steering_design import build_simple_wake_steering_lookup_table + +with open(os.path.join("inputs", "gch_whoc_example.yaml"), "r") as f: + floris_dict = yaml.safe_load(f) + +if __name__ == "__main__": + # Handle inputs + parser = argparse.ArgumentParser() + parser.add_argument("--yaw_offset_filename", default="yaw_offsets.pkl") + parser.add_argument("--input_wind_filename", default="amr_standin_data.csv") + + args = parser.parse_args() + + fmodel = FlorisModel(floris_dict) + + df_opt = build_simple_wake_steering_lookup_table( + fmodel, + wd_resolution=3.0, + ws_resolution=1.0, + ws_min=2.0, + ws_max=17.0, + minimum_yaw_angle=-25.0, + maximum_yaw_angle=25.0, + ) + + print("Optimization results:") + print(df_opt) + + df_opt.to_pickle(args.yaw_offset_filename) + + # Also, build an example external data file + total_time = 100 # seconds + dt = 0.5 + np.random.seed(0) + wind_directions = np.concatenate( + ( + 260 * np.ones(60), + np.linspace(260.0, 270.0, 80), + 270.0 + 5.0 * np.random.randn(round(total_time / dt) - 60 - 80), + ) + ) + df_data = pd.DataFrame( + data={ + "time": np.arange(0, total_time, dt), + "amr_wind_speed": 8.0 * np.ones_like(wind_directions), + "amr_wind_direction": wind_directions, + } + ) + + df_data.to_csv(args.input_wind_filename, index=False) diff --git a/examples/FAST.Farm_interface/inputs/FFFiles/5MW_Land_DLL_WTurb.T1.fst b/examples/FAST.Farm_interface/inputs/FFFiles/5MW_Land_DLL_WTurb.T1.fst new file mode 100644 index 00000000..004145fb --- /dev/null +++ b/examples/FAST.Farm_interface/inputs/FFFiles/5MW_Land_DLL_WTurb.T1.fst @@ -0,0 +1,73 @@ +------- OpenFAST EXAMPLE INPUT FILE ------------------------------------------- +FAST Certification - Test #18: NREL 5.0 MW Baseline Wind Turbine (Onshore) +---------------------- SIMULATION CONTROL -------------------------------------- +False Echo - Echo input data to .ech (flag) +"FATAL" AbortLevel - Error level when simulation should abort (string) {"WARNING", "SEVERE", "FATAL"} +600 TMax - Total run time (s) +0.00625 DT - Recommended module time step (s) +2 InterpOrder - Interpolation order for input/output time history (-) {1=linear, 2=quadratic} +0 NumCrctn - Number of correction iterations (-) {0=explicit calculation, i.e., no corrections} +99999 DT_UJac - Time between calls to get Jacobians (s) +1000000.0 UJacSclFact - Scaling factor used in Jacobians (-) +---------------------- FEATURE SWITCHES AND FLAGS ------------------------------ +1 CompElast - Compute structural dynamics (switch) {1=ElastoDyn; 2=ElastoDyn + BeamDyn for blades} +1 CompInflow - Compute inflow wind velocities (switch) {0=still air; 1=InflowWind; 2=external from OpenFOAM} +2 CompAero - Compute aerodynamic loads (switch) {0=None; 1=AeroDyn v14; 2=AeroDyn v15} +1 CompServo - Compute control and electrical-drive dynamics (switch) {0=None; 1=ServoDyn} +0 CompSeaSt - Compute sea state information (switch) {0=None; 1=SeaState} +0 CompHydro - Compute hydrodynamic loads (switch) {0=None; 1=HydroDyn} +0 CompSub - Compute sub-structural dynamics (switch) {0=None; 1=SubDyn; 2=External Platform MCKF} +0 CompMooring - Compute mooring system (switch) {0=None; 1=MAP++; 2=FEAMooring; 3=MoorDyn; 4=OrcaFlex} +0 CompIce - Compute ice loads (switch) {0=None; 1=IceFloe; 2=IceDyn} +0 MHK - MHK turbine type (switch) {0=Not an MHK turbine; 1=Fixed MHK turbine; 2=Floating MHK turbine} +---------------------- ENVIRONMENTAL CONDITIONS -------------------------------- +9.80665 Gravity - Gravitational acceleration (m/s^2) +1.225 AirDens - Air density (kg/m^3) +0 WtrDens - Water density (kg/m^3) +1.464e-05 KinVisc - Kinematic viscosity of working fluid (m^2/s) +335 SpdSound - Speed of sound in working fluid (m/s) +103500 Patm - Atmospheric pressure (Pa) [used only for an MHK turbine cavitation check] +1700 Pvap - Vapour pressure of working fluid (Pa) [used only for an MHK turbine cavitation check] +0 WtrDpth - Water depth (m) +0 MSL2SWL - Offset between still-water level and mean sea level (m) [positive upward] +---------------------- INPUT FILES --------------------------------------------- +"./NRELOffshrBsline5MW_Onshore_ElastoDyn.T1_mod.dat" EDFile - Name of file containing ElastoDyn input parameters (quoted string) +"unused" BDBldFile(1) - Name of file containing BeamDyn input parameters for blade 1 (quoted string) +"unused" BDBldFile(2) - Name of file containing BeamDyn input parameters for blade 2 (quoted string) +"unused" BDBldFile(3) - Name of file containing BeamDyn input parameters for blade 3 (quoted string) +"./NRELOffshrBsline5MW_InflowWind_Steady8mps.dat" InflowFile - Name of file containing inflow wind input parameters (quoted string) +"./NRELOffshrBsline5MW_Onshore_AeroDyn15.dat" AeroFile - Name of file containing aerodynamic input parameters (quoted string) +"./NRELOffshrBsline5MW_Onshore_ServoDyn.T1_mod.dat" ServoFile - Name of file containing control and electrical-drive input parameters (quoted string) +"unused" SeaStFile - Name of file containing sea state input parameters (quoted string) +"./unused" HydroFile - Name of file containing hydrodynamic input parameters (quoted string) +"unused" SubFile - Name of file containing sub-structural input parameters (quoted string) +"unused" MooringFile - Name of file containing mooring system input parameters (quoted string) +"unused" IceFile - Name of file containing ice input parameters (quoted string) +---------------------- OUTPUT -------------------------------------------------- +False SumPrint - Print summary data to ".sum" (flag) +5 SttsTime - Amount of time between screen status messages (s) +99999 ChkptTime - Amount of time between creating checkpoint files for potential restart (s) +"default" DT_Out - Time step for tabular output (s) (or "default") +0 TStart - Time to begin tabular output (s) +0 OutFileFmt - Format for tabular (time-marching) output file (switch) {0: uncompressed binary [.outb], 1: text file [.out], 2: binary file [.outb], 3: both 1 and 2} +True TabDelim - Use tab delimiters in text tabular output file? (flag) {uses spaces if false} +"ES10.3E2" OutFmt - Format used for text tabular output, excluding the time channel. Resulting field should be 10 characters. (quoted string) +---------------------- LINEARIZATION ------------------------------------------- +False Linearize - Linearization analysis (flag) +False CalcSteady - Calculate a steady-state periodic operating point before linearization? [unused if Linearize=False] (flag) +3 TrimCase - Controller parameter to be trimmed {1:yaw; 2:torque; 3:pitch} [used only if CalcSteady=True] (-) +0.001 TrimTol - Tolerance for the rotational speed convergence [used only if CalcSteady=True] (-) +0.01 TrimGain - Proportional gain for the rotational speed error (>0) [used only if CalcSteady=True] (rad/(rad/s) for yaw or pitch; Nm/(rad/s) for torque) +0 Twr_Kdmp - Damping factor for the tower [used only if CalcSteady=True] (N/(m/s)) +0 Bld_Kdmp - Damping factor for the blades [used only if CalcSteady=True] (N/(m/s)) +2 NLinTimes - Number of times to linearize (-) [>=1] [unused if Linearize=False] +30, 60 LinTimes - List of times at which to linearize (s) [1 to NLinTimes] [used only when Linearize=True and CalcSteady=False] +1 LinInputs - Inputs included in linearization (switch) {0=none; 1=standard; 2=all module inputs (debug)} [unused if Linearize=False] +1 LinOutputs - Outputs included in linearization (switch) {0=none; 1=from OutList(s); 2=all module outputs (debug)} [unused if Linearize=False] +False LinOutJac - Include full Jacobians in linearization output (for debug) (flag) [unused if Linearize=False; used only if LinInputs=LinOutputs=2] +False LinOutMod - Write module-level linearization output files in addition to output for full system? (flag) [unused if Linearize=False] +---------------------- VISUALIZATION ------------------------------------------ +0 WrVTK - VTK visualization data output: (switch) {0=none; 1=initialization data only; 2=animation; 3=mode shapes} +1 VTK_type - Type of VTK visualization data: (switch) {1=surfaces; 2=basic meshes (lines/points); 3=all meshes (debug)} [unused if WrVTK=0] +True VTK_fields - Write mesh fields to VTK data files? (flag) {true/false} [unused if WrVTK=0] +15 VTK_fps - Frame rate for VTK output (frames per second){will use closest integer multiple of DT} [used only if WrVTK=2 or WrVTK=3] \ No newline at end of file diff --git a/examples/FAST.Farm_interface/inputs/FFFiles/5MW_Land_DLL_WTurb.T2.fst b/examples/FAST.Farm_interface/inputs/FFFiles/5MW_Land_DLL_WTurb.T2.fst new file mode 100644 index 00000000..5b1f5d1d --- /dev/null +++ b/examples/FAST.Farm_interface/inputs/FFFiles/5MW_Land_DLL_WTurb.T2.fst @@ -0,0 +1,73 @@ +------- OpenFAST EXAMPLE INPUT FILE ------------------------------------------- +FAST Certification - Test #18: NREL 5.0 MW Baseline Wind Turbine (Onshore) +---------------------- SIMULATION CONTROL -------------------------------------- +False Echo - Echo input data to .ech (flag) +"FATAL" AbortLevel - Error level when simulation should abort (string) {"WARNING", "SEVERE", "FATAL"} +600 TMax - Total run time (s) +0.00625 DT - Recommended module time step (s) +2 InterpOrder - Interpolation order for input/output time history (-) {1=linear, 2=quadratic} +0 NumCrctn - Number of correction iterations (-) {0=explicit calculation, i.e., no corrections} +99999 DT_UJac - Time between calls to get Jacobians (s) +1000000.0 UJacSclFact - Scaling factor used in Jacobians (-) +---------------------- FEATURE SWITCHES AND FLAGS ------------------------------ +1 CompElast - Compute structural dynamics (switch) {1=ElastoDyn; 2=ElastoDyn + BeamDyn for blades} +1 CompInflow - Compute inflow wind velocities (switch) {0=still air; 1=InflowWind; 2=external from OpenFOAM} +2 CompAero - Compute aerodynamic loads (switch) {0=None; 1=AeroDyn v14; 2=AeroDyn v15} +1 CompServo - Compute control and electrical-drive dynamics (switch) {0=None; 1=ServoDyn} +0 CompSeaSt - Compute sea state information (switch) {0=None; 1=SeaState} +0 CompHydro - Compute hydrodynamic loads (switch) {0=None; 1=HydroDyn} +0 CompSub - Compute sub-structural dynamics (switch) {0=None; 1=SubDyn; 2=External Platform MCKF} +0 CompMooring - Compute mooring system (switch) {0=None; 1=MAP++; 2=FEAMooring; 3=MoorDyn; 4=OrcaFlex} +0 CompIce - Compute ice loads (switch) {0=None; 1=IceFloe; 2=IceDyn} +0 MHK - MHK turbine type (switch) {0=Not an MHK turbine; 1=Fixed MHK turbine; 2=Floating MHK turbine} +---------------------- ENVIRONMENTAL CONDITIONS -------------------------------- +9.80665 Gravity - Gravitational acceleration (m/s^2) +1.225 AirDens - Air density (kg/m^3) +0 WtrDens - Water density (kg/m^3) +1.464e-05 KinVisc - Kinematic viscosity of working fluid (m^2/s) +335 SpdSound - Speed of sound in working fluid (m/s) +103500 Patm - Atmospheric pressure (Pa) [used only for an MHK turbine cavitation check] +1700 Pvap - Vapour pressure of working fluid (Pa) [used only for an MHK turbine cavitation check] +0 WtrDpth - Water depth (m) +0 MSL2SWL - Offset between still-water level and mean sea level (m) [positive upward] +---------------------- INPUT FILES --------------------------------------------- +"./NRELOffshrBsline5MW_Onshore_ElastoDyn.T2_mod.dat" EDFile - Name of file containing ElastoDyn input parameters (quoted string) +"unused" BDBldFile(1) - Name of file containing BeamDyn input parameters for blade 1 (quoted string) +"unused" BDBldFile(2) - Name of file containing BeamDyn input parameters for blade 2 (quoted string) +"unused" BDBldFile(3) - Name of file containing BeamDyn input parameters for blade 3 (quoted string) +"./NRELOffshrBsline5MW_InflowWind_Steady8mps.dat" InflowFile - Name of file containing inflow wind input parameters (quoted string) +"./NRELOffshrBsline5MW_Onshore_AeroDyn15.dat" AeroFile - Name of file containing aerodynamic input parameters (quoted string) +"./NRELOffshrBsline5MW_Onshore_ServoDyn.T2_mod.dat" ServoFile - Name of file containing control and electrical-drive input parameters (quoted string) +"unused" SeaStFile - Name of file containing sea state input parameters (quoted string) +"./unused" HydroFile - Name of file containing hydrodynamic input parameters (quoted string) +"unused" SubFile - Name of file containing sub-structural input parameters (quoted string) +"unused" MooringFile - Name of file containing mooring system input parameters (quoted string) +"unused" IceFile - Name of file containing ice input parameters (quoted string) +---------------------- OUTPUT -------------------------------------------------- +False SumPrint - Print summary data to ".sum" (flag) +5 SttsTime - Amount of time between screen status messages (s) +99999 ChkptTime - Amount of time between creating checkpoint files for potential restart (s) +"default" DT_Out - Time step for tabular output (s) (or "default") +0 TStart - Time to begin tabular output (s) +0 OutFileFmt - Format for tabular (time-marching) output file (switch) {0: uncompressed binary [.outb], 1: text file [.out], 2: binary file [.outb], 3: both 1 and 2} +True TabDelim - Use tab delimiters in text tabular output file? (flag) {uses spaces if false} +"ES10.3E2" OutFmt - Format used for text tabular output, excluding the time channel. Resulting field should be 10 characters. (quoted string) +---------------------- LINEARIZATION ------------------------------------------- +False Linearize - Linearization analysis (flag) +False CalcSteady - Calculate a steady-state periodic operating point before linearization? [unused if Linearize=False] (flag) +3 TrimCase - Controller parameter to be trimmed {1:yaw; 2:torque; 3:pitch} [used only if CalcSteady=True] (-) +0.001 TrimTol - Tolerance for the rotational speed convergence [used only if CalcSteady=True] (-) +0.01 TrimGain - Proportional gain for the rotational speed error (>0) [used only if CalcSteady=True] (rad/(rad/s) for yaw or pitch; Nm/(rad/s) for torque) +0 Twr_Kdmp - Damping factor for the tower [used only if CalcSteady=True] (N/(m/s)) +0 Bld_Kdmp - Damping factor for the blades [used only if CalcSteady=True] (N/(m/s)) +2 NLinTimes - Number of times to linearize (-) [>=1] [unused if Linearize=False] +30, 60 LinTimes - List of times at which to linearize (s) [1 to NLinTimes] [used only when Linearize=True and CalcSteady=False] +1 LinInputs - Inputs included in linearization (switch) {0=none; 1=standard; 2=all module inputs (debug)} [unused if Linearize=False] +1 LinOutputs - Outputs included in linearization (switch) {0=none; 1=from OutList(s); 2=all module outputs (debug)} [unused if Linearize=False] +False LinOutJac - Include full Jacobians in linearization output (for debug) (flag) [unused if Linearize=False; used only if LinInputs=LinOutputs=2] +False LinOutMod - Write module-level linearization output files in addition to output for full system? (flag) [unused if Linearize=False] +---------------------- VISUALIZATION ------------------------------------------ +0 WrVTK - VTK visualization data output: (switch) {0=none; 1=initialization data only; 2=animation; 3=mode shapes} +1 VTK_type - Type of VTK visualization data: (switch) {1=surfaces; 2=basic meshes (lines/points); 3=all meshes (debug)} [unused if WrVTK=0] +True VTK_fields - Write mesh fields to VTK data files? (flag) {true/false} [unused if WrVTK=0] +15 VTK_fps - Frame rate for VTK output (frames per second){will use closest integer multiple of DT} [used only if WrVTK=2 or WrVTK=3] \ No newline at end of file diff --git a/examples/FAST.Farm_interface/inputs/FFFiles/5MW_Land_DLL_WTurb.T3.fst b/examples/FAST.Farm_interface/inputs/FFFiles/5MW_Land_DLL_WTurb.T3.fst new file mode 100644 index 00000000..b17b9ebf --- /dev/null +++ b/examples/FAST.Farm_interface/inputs/FFFiles/5MW_Land_DLL_WTurb.T3.fst @@ -0,0 +1,73 @@ +------- OpenFAST EXAMPLE INPUT FILE ------------------------------------------- +FAST Certification - Test #18: NREL 5.0 MW Baseline Wind Turbine (Onshore) +---------------------- SIMULATION CONTROL -------------------------------------- +False Echo - Echo input data to .ech (flag) +"FATAL" AbortLevel - Error level when simulation should abort (string) {"WARNING", "SEVERE", "FATAL"} +600 TMax - Total run time (s) +0.00625 DT - Recommended module time step (s) +2 InterpOrder - Interpolation order for input/output time history (-) {1=linear, 2=quadratic} +0 NumCrctn - Number of correction iterations (-) {0=explicit calculation, i.e., no corrections} +99999 DT_UJac - Time between calls to get Jacobians (s) +1000000.0 UJacSclFact - Scaling factor used in Jacobians (-) +---------------------- FEATURE SWITCHES AND FLAGS ------------------------------ +1 CompElast - Compute structural dynamics (switch) {1=ElastoDyn; 2=ElastoDyn + BeamDyn for blades} +1 CompInflow - Compute inflow wind velocities (switch) {0=still air; 1=InflowWind; 2=external from OpenFOAM} +2 CompAero - Compute aerodynamic loads (switch) {0=None; 1=AeroDyn v14; 2=AeroDyn v15} +1 CompServo - Compute control and electrical-drive dynamics (switch) {0=None; 1=ServoDyn} +0 CompSeaSt - Compute sea state information (switch) {0=None; 1=SeaState} +0 CompHydro - Compute hydrodynamic loads (switch) {0=None; 1=HydroDyn} +0 CompSub - Compute sub-structural dynamics (switch) {0=None; 1=SubDyn; 2=External Platform MCKF} +0 CompMooring - Compute mooring system (switch) {0=None; 1=MAP++; 2=FEAMooring; 3=MoorDyn; 4=OrcaFlex} +0 CompIce - Compute ice loads (switch) {0=None; 1=IceFloe; 2=IceDyn} +0 MHK - MHK turbine type (switch) {0=Not an MHK turbine; 1=Fixed MHK turbine; 2=Floating MHK turbine} +---------------------- ENVIRONMENTAL CONDITIONS -------------------------------- +9.80665 Gravity - Gravitational acceleration (m/s^2) +1.225 AirDens - Air density (kg/m^3) +0 WtrDens - Water density (kg/m^3) +1.464e-05 KinVisc - Kinematic viscosity of working fluid (m^2/s) +335 SpdSound - Speed of sound in working fluid (m/s) +103500 Patm - Atmospheric pressure (Pa) [used only for an MHK turbine cavitation check] +1700 Pvap - Vapour pressure of working fluid (Pa) [used only for an MHK turbine cavitation check] +0 WtrDpth - Water depth (m) +0 MSL2SWL - Offset between still-water level and mean sea level (m) [positive upward] +---------------------- INPUT FILES --------------------------------------------- +"./NRELOffshrBsline5MW_Onshore_ElastoDyn.T3_mod.dat" EDFile - Name of file containing ElastoDyn input parameters (quoted string) +"unused" BDBldFile(1) - Name of file containing BeamDyn input parameters for blade 1 (quoted string) +"unused" BDBldFile(2) - Name of file containing BeamDyn input parameters for blade 2 (quoted string) +"unused" BDBldFile(3) - Name of file containing BeamDyn input parameters for blade 3 (quoted string) +"./NRELOffshrBsline5MW_InflowWind_Steady8mps.dat" InflowFile - Name of file containing inflow wind input parameters (quoted string) +"./NRELOffshrBsline5MW_Onshore_AeroDyn15.dat" AeroFile - Name of file containing aerodynamic input parameters (quoted string) +"./NRELOffshrBsline5MW_Onshore_ServoDyn.T3_mod.dat" ServoFile - Name of file containing control and electrical-drive input parameters (quoted string) +"unused" SeaStFile - Name of file containing sea state input parameters (quoted string) +"./unused" HydroFile - Name of file containing hydrodynamic input parameters (quoted string) +"unused" SubFile - Name of file containing sub-structural input parameters (quoted string) +"unused" MooringFile - Name of file containing mooring system input parameters (quoted string) +"unused" IceFile - Name of file containing ice input parameters (quoted string) +---------------------- OUTPUT -------------------------------------------------- +False SumPrint - Print summary data to ".sum" (flag) +5 SttsTime - Amount of time between screen status messages (s) +99999 ChkptTime - Amount of time between creating checkpoint files for potential restart (s) +"default" DT_Out - Time step for tabular output (s) (or "default") +0 TStart - Time to begin tabular output (s) +0 OutFileFmt - Format for tabular (time-marching) output file (switch) {0: uncompressed binary [.outb], 1: text file [.out], 2: binary file [.outb], 3: both 1 and 2} +True TabDelim - Use tab delimiters in text tabular output file? (flag) {uses spaces if false} +"ES10.3E2" OutFmt - Format used for text tabular output, excluding the time channel. Resulting field should be 10 characters. (quoted string) +---------------------- LINEARIZATION ------------------------------------------- +False Linearize - Linearization analysis (flag) +False CalcSteady - Calculate a steady-state periodic operating point before linearization? [unused if Linearize=False] (flag) +3 TrimCase - Controller parameter to be trimmed {1:yaw; 2:torque; 3:pitch} [used only if CalcSteady=True] (-) +0.001 TrimTol - Tolerance for the rotational speed convergence [used only if CalcSteady=True] (-) +0.01 TrimGain - Proportional gain for the rotational speed error (>0) [used only if CalcSteady=True] (rad/(rad/s) for yaw or pitch; Nm/(rad/s) for torque) +0 Twr_Kdmp - Damping factor for the tower [used only if CalcSteady=True] (N/(m/s)) +0 Bld_Kdmp - Damping factor for the blades [used only if CalcSteady=True] (N/(m/s)) +2 NLinTimes - Number of times to linearize (-) [>=1] [unused if Linearize=False] +30, 60 LinTimes - List of times at which to linearize (s) [1 to NLinTimes] [used only when Linearize=True and CalcSteady=False] +1 LinInputs - Inputs included in linearization (switch) {0=none; 1=standard; 2=all module inputs (debug)} [unused if Linearize=False] +1 LinOutputs - Outputs included in linearization (switch) {0=none; 1=from OutList(s); 2=all module outputs (debug)} [unused if Linearize=False] +False LinOutJac - Include full Jacobians in linearization output (for debug) (flag) [unused if Linearize=False; used only if LinInputs=LinOutputs=2] +False LinOutMod - Write module-level linearization output files in addition to output for full system? (flag) [unused if Linearize=False] +---------------------- VISUALIZATION ------------------------------------------ +0 WrVTK - VTK visualization data output: (switch) {0=none; 1=initialization data only; 2=animation; 3=mode shapes} +1 VTK_type - Type of VTK visualization data: (switch) {1=surfaces; 2=basic meshes (lines/points); 3=all meshes (debug)} [unused if WrVTK=0] +True VTK_fields - Write mesh fields to VTK data files? (flag) {true/false} [unused if WrVTK=0] +15 VTK_fps - Frame rate for VTK output (frames per second){will use closest integer multiple of DT} [used only if WrVTK=2 or WrVTK=3] \ No newline at end of file diff --git a/examples/FAST.Farm_interface/inputs/FFFiles/Airfoils/Cylinder1.dat b/examples/FAST.Farm_interface/inputs/FFFiles/Airfoils/Cylinder1.dat new file mode 100644 index 00000000..d9e59b23 --- /dev/null +++ b/examples/FAST.Farm_interface/inputs/FFFiles/Airfoils/Cylinder1.dat @@ -0,0 +1,59 @@ +! ------------ AirfoilInfo v1.01.x Input File ---------------------------------- +! Round root section with a Cd of 0.50 +! Made by Jason Jonkman +! note that this file uses Marshall Buhl's new input file processing; start all comment lines with ! +! ------------------------------------------------------------------------------ +"DEFAULT" InterpOrd ! Interpolation order to use for quasi-steady table lookup {1=linear; 3=cubic spline; "default"} [default=1] + 1 NonDimArea ! The non-dimensional area of the airfoil (area/chord^2) (set to 1.0 if unsure or unneeded) +@"Cylinder1_coords.txt" NumCoords ! The number of coordinates in the airfoil shape file. Set to zero if coordinates not included. +"unused" BL_file ! The file name including the boundary layer characteristics of the profile. Ignored if the aeroacoustic module is not called. + 1 NumTabs ! Number of airfoil tables in this file. +! ------------------------------------------------------------------------------ +! data for table 1 +! ------------------------------------------------------------------------------ + 0.75 Re ! Reynolds number in millions + 0 UserProp ! User property (control) setting +True InclUAdata ! Is unsteady aerodynamics data included in this table? If TRUE, then include 30 UA coefficients below this line +!........................................ + 0 alpha0 ! 0-lift angle of attack, depends on airfoil. + 0 alpha1 ! Angle of attack at f=0.7, (approximately the stall angle) for AOA>alpha0. (deg) + 0 alpha2 ! Angle of attack at f=0.7, (approximately the stall angle) for AOA1] + 0 S2 ! Constant in the f curve best-fit for AOA> alpha1; by definition it depends on the airfoil. [ignored if UAMod<>1] + 0 S3 ! Constant in the f curve best-fit for alpha2<=AOA< alpha0; by definition it depends on the airfoil. [ignored if UAMod<>1] + 0 S4 ! Constant in the f curve best-fit for AOA< alpha2; by definition it depends on the airfoil. [ignored if UAMod<>1] + 0 Cn1 ! Critical value of C0n at leading edge separation. It should be extracted from airfoil data at a given Mach and Reynolds number. It can be calculated from the static value of Cn at either the break in the pitching moment or the loss of chord force at the onset of stall. It is close to the condition of maximum lift of the airfoil at low Mach numbers. + 0 Cn2 ! As Cn1 for negative AOAs. + 0.19 St_sh ! Strouhal's shedding frequency constant. [default = 0.19] + 0.5 Cd0 ! 2D drag coefficient value at 0-lift. + 0 Cm0 ! 2D pitching moment coefficient about 1/4-chord location, at 0-lift, positive if nose up. [If the aerodynamics coefficients table does not include a column for Cm, this needs to be set to 0.0] + 0 k0 ! Constant in the \hat(x)_cp curve best-fit; = (\hat(x)_AC-0.25). [ignored if UAMod<>1] + 0 k1 ! Constant in the \hat(x)_cp curve best-fit. [ignored if UAMod<>1] + 0 k2 ! Constant in the \hat(x)_cp curve best-fit. [ignored if UAMod<>1] + 0 k3 ! Constant in the \hat(x)_cp curve best-fit. [ignored if UAMod<>1] + 0 k1_hat ! Constant in the expression of Cc due to leading edge vortex effects. [ignored if UAMod<>1] + 0.2 x_cp_bar ! Constant in the expression of \hat(x)_cp^v. [ignored if UAMod<>1, default = 0.2] +"DEFAULT" UACutout ! Angle of attack above which unsteady aerodynamics are disabled (deg). [Specifying the string "Default" sets UACutout to 45 degrees] +"DEFAULT" filtCutOff ! Reduced frequency cut-off for low-pass filtering the AoA input to UA, as well as the 1st and 2nd derivatives (-) [default = 0.5] +!........................................ +! Table of aerodynamics coefficients + 3 NumAlf ! Number of data lines in the following table +! Alpha Cl Cd Cm +! (deg) (-) (-) (-) + -180.00 0.000 0.5000 0.0 + 0.00 0.000 0.5000 0.0 + 180.00 0.000 0.5000 0.0 +! ------------------------------------------------------------------------------ + diff --git a/examples/FAST.Farm_interface/inputs/FFFiles/Airfoils/Cylinder1_coords.txt b/examples/FAST.Farm_interface/inputs/FFFiles/Airfoils/Cylinder1_coords.txt new file mode 100644 index 00000000..30663b70 --- /dev/null +++ b/examples/FAST.Farm_interface/inputs/FFFiles/Airfoils/Cylinder1_coords.txt @@ -0,0 +1,407 @@ + 400 NumCoords ! The number of coordinates in the airfoil shape file (including an extra coordinate for airfoil reference). Set to zero if coordinates not included. +! ......... x-y coordinates are next if NumCoords > 0 ............. +! x-y coordinate of airfoil reference +! x/c y/c +0.5 0 +! coordinates of airfoil shape +! cylinder (interpolated to 399 points) +! x/c y/c +1.000000 0.000000 +0.996600 0.058210 +0.993140 0.082541 +0.989610 0.101400 +0.986010 0.117449 +0.982350 0.131676 +0.978630 0.144614 +0.974840 0.156611 +0.970980 0.167863 +0.967060 0.178480 +0.963070 0.188590 +0.959020 0.198244 +0.954900 0.207523 +0.950720 0.216452 +0.946470 0.225088 +0.942160 0.233441 +0.937780 0.241555 +0.933330 0.249450 +0.928820 0.257125 +0.924250 0.264598 +0.919610 0.271896 +0.914900 0.279030 +0.910130 0.285995 +0.905290 0.292814 +0.900390 0.299479 +0.895420 0.306011 +0.890390 0.312403 +0.885290 0.318672 +0.880130 0.324809 +0.874900 0.330832 +0.869610 0.336732 +0.864250 0.342523 +0.858820 0.348207 +0.853330 0.353777 +0.847780 0.359234 +0.842160 0.364591 +0.836470 0.369849 +0.830720 0.374999 +0.824900 0.380053 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-0.082541 +0.996600 -0.058210 +1.000000 0.000000 diff --git a/examples/FAST.Farm_interface/inputs/FFFiles/Airfoils/Cylinder2.dat b/examples/FAST.Farm_interface/inputs/FFFiles/Airfoils/Cylinder2.dat new file mode 100644 index 00000000..f6e6a9fe --- /dev/null +++ b/examples/FAST.Farm_interface/inputs/FFFiles/Airfoils/Cylinder2.dat @@ -0,0 +1,60 @@ +! ------------ AirfoilInfo v1.01.x Input File ---------------------------------- +! Round root section with a Cd of 0.35 +! Made by Jason Jonkman +! note that this file uses Marshall Buhl's new input file processing; start all comment lines with ! +! ------------------------------------------------------------------------------ +"DEFAULT" InterpOrd ! Interpolation order to use for quasi-steady table lookup {1=linear; 3=cubic spline; "default"} [default=1] + 1 NonDimArea ! The non-dimensional area of the airfoil (area/chord^2) (set to 1.0 if unsure or unneeded) +@"Cylinder2_coords.txt" NumCoords ! The number of coordinates in the airfoil shape file. Set to zero if coordinates not included. +! ......... x-y coordinates are next if NumCoords > 0 ............. +"unused" BL_file ! The file name including the boundary layer characteristics of the profile. Ignored if the aeroacoustic module is not called. + 1 NumTabs ! Number of airfoil tables in this file. +! ------------------------------------------------------------------------------ +! data for table 1 +! ------------------------------------------------------------------------------ + 0.75 Re ! Reynolds number in millions + 0 UserProp ! User property (control) setting +True InclUAdata ! Is unsteady aerodynamics data included in this table? If TRUE, then include 30 UA coefficients below this line +!........................................ + 0 alpha0 ! 0-lift angle of attack, depends on airfoil. + 0 alpha1 ! Angle of attack at f=0.7, (approximately the stall angle) for AOA>alpha0. (deg) + 0 alpha2 ! Angle of attack at f=0.7, (approximately the stall angle) for AOA1] + 0 S2 ! Constant in the f curve best-fit for AOA> alpha1; by definition it depends on the airfoil. [ignored if UAMod<>1] + 0 S3 ! Constant in the f curve best-fit for alpha2<=AOA< alpha0; by definition it depends on the airfoil. [ignored if UAMod<>1] + 0 S4 ! Constant in the f curve best-fit for AOA< alpha2; by definition it depends on the airfoil. [ignored if UAMod<>1] + 0 Cn1 ! Critical value of C0n at leading edge separation. It should be extracted from airfoil data at a given Mach and Reynolds number. It can be calculated from the static value of Cn at either the break in the pitching moment or the loss of chord force at the onset of stall. It is close to the condition of maximum lift of the airfoil at low Mach numbers. + 0 Cn2 ! As Cn1 for negative AOAs. + 0.19 St_sh ! Strouhal's shedding frequency constant. [default = 0.19] + 0.35 Cd0 ! 2D drag coefficient value at 0-lift. + 0 Cm0 ! 2D pitching moment coefficient about 1/4-chord location, at 0-lift, positive if nose up. [If the aerodynamics coefficients table does not include a column for Cm, this needs to be set to 0.0] + 0 k0 ! Constant in the \hat(x)_cp curve best-fit; = (\hat(x)_AC-0.25). [ignored if UAMod<>1] + 0 k1 ! Constant in the \hat(x)_cp curve best-fit. [ignored if UAMod<>1] + 0 k2 ! Constant in the \hat(x)_cp curve best-fit. [ignored if UAMod<>1] + 0 k3 ! Constant in the \hat(x)_cp curve best-fit. [ignored if UAMod<>1] + 0 k1_hat ! Constant in the expression of Cc due to leading edge vortex effects. [ignored if UAMod<>1] + 0.2 x_cp_bar ! Constant in the expression of \hat(x)_cp^v. [ignored if UAMod<>1, default = 0.2] +"DEFAULT" UACutout ! Angle of attack above which unsteady aerodynamics are disabled (deg). [Specifying the string "Default" sets UACutout to 45 degrees] +"DEFAULT" filtCutOff ! Reduced frequency cut-off for low-pass filtering the AoA input to UA, as well as the 1st and 2nd derivatives (-) [default = 0.5] +!........................................ +! Table of aerodynamics coefficients + 3 NumAlf ! Number of data lines in the following table +! Alpha Cl Cd Cm +! (deg) (-) (-) (-) + -180.00 0.000 0.3500 0.0 + 0.00 0.000 0.3500 0.0 + 180.00 0.000 0.3500 0.0 +! ------------------------------------------------------------------------------ + diff --git a/examples/FAST.Farm_interface/inputs/FFFiles/Airfoils/Cylinder2_coords.txt b/examples/FAST.Farm_interface/inputs/FFFiles/Airfoils/Cylinder2_coords.txt new file mode 100644 index 00000000..ba5741b6 --- /dev/null +++ b/examples/FAST.Farm_interface/inputs/FFFiles/Airfoils/Cylinder2_coords.txt @@ -0,0 +1,407 @@ + 400 NumCoords ! The number of coordinates in the airfoil shape file (including an extra coordinate for airfoil reference). Set to zero if coordinates not included. +! ......... x-y coordinates are next if NumCoords > 0 ............. +! x-y coordinate of airfoil reference +! x/c y/c +0.41667 0 +! coordinates of airfoil shape +! cylinder (interpolated to 399 points) +! x/c y/c +1.000000 0.000000 +0.996600 0.058210 +0.993140 0.082541 +0.989610 0.101400 +0.986010 0.117449 +0.982350 0.131676 +0.978630 0.144614 +0.974840 0.156611 +0.970980 0.167863 +0.967060 0.178480 +0.963070 0.188590 +0.959020 0.198244 +0.954900 0.207523 +0.950720 0.216452 +0.946470 0.225088 +0.942160 0.233441 +0.937780 0.241555 +0.933330 0.249450 +0.928820 0.257125 +0.924250 0.264598 +0.919610 0.271896 +0.914900 0.279030 +0.910130 0.285995 +0.905290 0.292814 +0.900390 0.299479 +0.895420 0.306011 +0.890390 0.312403 +0.885290 0.318672 +0.880130 0.324809 +0.874900 0.330832 +0.869610 0.336732 +0.864250 0.342523 +0.858820 0.348207 +0.853330 0.353777 +0.847780 0.359234 +0.842160 0.364591 +0.836470 0.369849 +0.830720 0.374999 +0.824900 0.380053 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-0.082541 +0.996600 -0.058210 +1.000000 0.000000 diff --git a/examples/FAST.Farm_interface/inputs/FFFiles/Airfoils/DU21_A17.dat b/examples/FAST.Farm_interface/inputs/FFFiles/Airfoils/DU21_A17.dat new file mode 100644 index 00000000..9fb97f0d --- /dev/null +++ b/examples/FAST.Farm_interface/inputs/FFFiles/Airfoils/DU21_A17.dat @@ -0,0 +1,196 @@ +! ------------ AirfoilInfo v1.01.x Input File ---------------------------------- +! DU21 airfoil with an aspect ratio of 17. Original -180 to 180deg Cl, Cd, and Cm versus AOA data taken from Appendix A of DOWEC document 10046_009.pdf (numerical values obtained from Koert Lindenburg of ECN). +! Cl and Cd values corrected for rotational stall delay and Cd values corrected using the Viterna method for 0 to 90deg AOA by Jason Jonkman using AirfoilPrep_v2p0.xls. +! note that this file uses Marshall Buhl's new input file processing; start all comment lines with ! +! ------------------------------------------------------------------------------ +"DEFAULT" InterpOrd ! Interpolation order to use for quasi-steady table lookup {1=linear; 3=cubic spline; "default"} [default=1] + 1 NonDimArea ! The non-dimensional area of the airfoil (area/chord^2) (set to 1.0 if unsure or unneeded) +@"DU21_A17_coords.txt" NumCoords ! The number of coordinates in the airfoil shape file. Set to zero if coordinates not included. +"unused" BL_file ! The file name including the boundary layer characteristics of the profile. Ignored if the aeroacoustic module is not called. + 1 NumTabs ! Number of airfoil tables in this file. +! ------------------------------------------------------------------------------ +! data for table 1 +! ------------------------------------------------------------------------------ + 0.75 Re ! Reynolds number in millions + 0 UserProp ! User property (control) setting +True InclUAdata ! Is unsteady aerodynamics data included in this table? If TRUE, then include 30 UA coefficients below this line +!........................................ + -4.2 alpha0 ! 0-lift angle of attack, depends on airfoil. + 8 alpha1 ! Angle of attack at f=0.7, (approximately the stall angle) for AOA>alpha0. (deg) + -8 alpha2 ! Angle of attack at f=0.7, (approximately the stall angle) for AOA1] + 0 S2 ! Constant in the f curve best-fit for AOA> alpha1; by definition it depends on the airfoil. [ignored if UAMod<>1] + 0 S3 ! Constant in the f curve best-fit for alpha2<=AOA< alpha0; by definition it depends on the airfoil. [ignored if UAMod<>1] + 0 S4 ! Constant in the f curve best-fit for AOA< alpha2; by definition it depends on the airfoil. [ignored if UAMod<>1] + 1.4144 Cn1 ! Critical value of C0n at leading edge separation. It should be extracted from airfoil data at a given Mach and Reynolds number. It can be calculated from the static value of Cn at either the break in the pitching moment or the loss of chord force at the onset of stall. It is close to the condition of maximum lift of the airfoil at low Mach numbers. + -0.5324 Cn2 ! As Cn1 for negative AOAs. + 0.19 St_sh ! Strouhal's shedding frequency constant. [default = 0.19] + 0.006 Cd0 ! 2D drag coefficient value at 0-lift. + -0.121 Cm0 ! 2D pitching moment coefficient about 1/4-chord location, at 0-lift, positive if nose up. [If the aerodynamics coefficients table does not include a column for Cm, this needs to be set to 0.0] + 0 k0 ! Constant in the \hat(x)_cp curve best-fit; = (\hat(x)_AC-0.25). [ignored if UAMod<>1] + 0 k1 ! Constant in the \hat(x)_cp curve best-fit. [ignored if UAMod<>1] + 0 k2 ! Constant in the \hat(x)_cp curve best-fit. [ignored if UAMod<>1] + 0 k3 ! Constant in the \hat(x)_cp curve best-fit. [ignored if UAMod<>1] + 0 k1_hat ! Constant in the expression of Cc due to leading edge vortex effects. [ignored if UAMod<>1] + 0.2 x_cp_bar ! Constant in the expression of \hat(x)_cp^v. [ignored if UAMod<>1, default = 0.2] +"DEFAULT" UACutout ! Angle of attack above which unsteady aerodynamics are disabled (deg). [Specifying the string "Default" sets UACutout to 45 degrees] +"DEFAULT" filtCutOff ! Reduced frequency cut-off for low-pass filtering the AoA input to UA, as well as the 1st and 2nd derivatives (-) [default = 0.5] +!........................................ +! Table of aerodynamics coefficients + 142 NumAlf ! Number of data lines in the following table +! Alpha Cl Cd Cm +! (deg) (-) (-) (-) + -180.00 0.000 0.0185 0.0000 + -175.00 0.394 0.0332 0.1978 + -170.00 0.788 0.0945 0.3963 + -160.00 0.670 0.2809 0.2738 + -155.00 0.749 0.3932 0.3118 + -150.00 0.797 0.5112 0.3413 + -145.00 0.818 0.6309 0.3636 + -140.00 0.813 0.7485 0.3799 + -135.00 0.786 0.8612 0.3911 + -130.00 0.739 0.9665 0.3980 + -125.00 0.675 1.0625 0.4012 + -120.00 0.596 1.1476 0.4014 + -115.00 0.505 1.2206 0.3990 + -110.00 0.403 1.2805 0.3943 + -105.00 0.294 1.3265 0.3878 + -100.00 0.179 1.3582 0.3796 + -95.00 0.060 1.3752 0.3700 + -90.00 -0.060 1.3774 0.3591 + -85.00 -0.179 1.3648 0.3471 + -80.00 -0.295 1.3376 0.3340 + -75.00 -0.407 1.2962 0.3199 + -70.00 -0.512 1.2409 0.3049 + -65.00 -0.608 1.1725 0.2890 + -60.00 -0.693 1.0919 0.2722 + -55.00 -0.764 1.0002 0.2545 + -50.00 -0.820 0.8990 0.2359 + -45.00 -0.857 0.7900 0.2163 + -40.00 -0.875 0.6754 0.1958 + -35.00 -0.869 0.5579 0.1744 + -30.00 -0.838 0.4405 0.1520 + -25.00 -0.791 0.3256 0.1262 + -24.00 -0.794 0.3013 0.1170 + -23.00 -0.805 0.2762 0.1059 + -22.00 -0.821 0.2506 0.0931 + -21.00 -0.843 0.2246 0.0788 + -20.00 -0.869 0.1983 0.0631 + -19.00 -0.899 0.1720 0.0464 + -18.00 -0.931 0.1457 0.0286 + -17.00 -0.964 0.1197 0.0102 + -16.00 -0.999 0.0940 -0.0088 + -15.00 -1.033 0.0689 -0.0281 + -14.50 -1.050 0.0567 -0.0378 + -12.01 -0.953 0.0271 -0.0349 + -11.00 -0.900 0.0303 -0.0361 + -9.98 -0.827 0.0287 -0.0464 + -8.12 -0.536 0.0124 -0.0821 + -7.62 -0.467 0.0109 -0.0924 + -7.11 -0.393 0.0092 -0.1015 + -6.60 -0.323 0.0083 -0.1073 + -6.50 -0.311 0.0089 -0.1083 + -6.00 -0.245 0.0082 -0.1112 + -5.50 -0.178 0.0074 -0.1146 + -5.00 -0.113 0.0069 -0.1172 + -4.50 -0.048 0.0065 -0.1194 + -4.00 0.016 0.0063 -0.1213 + -3.50 0.080 0.0061 -0.1232 + -3.00 0.145 0.0058 -0.1252 + -2.50 0.208 0.0057 -0.1268 + -2.00 0.270 0.0057 -0.1282 + -1.50 0.333 0.0057 -0.1297 + -1.00 0.396 0.0057 -0.1310 + -0.50 0.458 0.0057 -0.1324 + 0.00 0.521 0.0057 -0.1337 + 0.50 0.583 0.0057 -0.1350 + 1.00 0.645 0.0058 -0.1363 + 1.50 0.706 0.0058 -0.1374 + 2.00 0.768 0.0059 -0.1385 + 2.50 0.828 0.0061 -0.1395 + 3.00 0.888 0.0063 -0.1403 + 3.50 0.948 0.0066 -0.1406 + 4.00 0.996 0.0071 -0.1398 + 4.50 1.046 0.0079 -0.1390 + 5.00 1.095 0.0090 -0.1378 + 5.50 1.145 0.0103 -0.1369 + 6.00 1.192 0.0113 -0.1353 + 6.50 1.239 0.0122 -0.1338 + 7.00 1.283 0.0131 -0.1317 + 7.50 1.324 0.0139 -0.1291 + 8.00 1.358 0.0147 -0.1249 + 8.50 1.385 0.0158 -0.1213 + 9.00 1.403 0.0181 -0.1177 + 9.50 1.401 0.0211 -0.1142 + 10.00 1.358 0.0255 -0.1103 + 10.50 1.313 0.0301 -0.1066 + 11.00 1.287 0.0347 -0.1032 + 11.50 1.274 0.0401 -0.1002 + 12.00 1.272 0.0468 -0.0971 + 12.50 1.273 0.0545 -0.0940 + 13.00 1.273 0.0633 -0.0909 + 13.50 1.273 0.0722 -0.0883 + 14.00 1.272 0.0806 -0.0865 + 14.50 1.273 0.0900 -0.0854 + 15.00 1.275 0.0987 -0.0849 + 15.50 1.281 0.1075 -0.0847 + 16.00 1.284 0.1170 -0.0850 + 16.50 1.296 0.1270 -0.0858 + 17.00 1.306 0.1368 -0.0869 + 17.50 1.308 0.1464 -0.0883 + 18.00 1.308 0.1562 -0.0901 + 18.50 1.308 0.1664 -0.0922 + 19.00 1.308 0.1770 -0.0949 + 19.50 1.307 0.1878 -0.0980 + 20.00 1.311 0.1987 -0.1017 + 20.50 1.325 0.2100 -0.1059 + 21.00 1.324 0.2214 -0.1105 + 22.00 1.277 0.2499 -0.1172 + 23.00 1.229 0.2786 -0.1239 + 24.00 1.182 0.3077 -0.1305 + 25.00 1.136 0.3371 -0.1370 + 26.00 1.093 0.3664 -0.1433 + 28.00 1.017 0.4246 -0.1556 + 30.00 0.962 0.4813 -0.1671 + 32.00 0.937 0.5356 -0.1778 + 35.00 0.947 0.6127 -0.1923 + 40.00 0.950 0.7396 -0.2154 + 45.00 0.928 0.8623 -0.2374 + 50.00 0.884 0.9781 -0.2583 + 55.00 0.821 1.0846 -0.2782 + 60.00 0.740 1.1796 -0.2971 + 65.00 0.646 1.2617 -0.3149 + 70.00 0.540 1.3297 -0.3318 + 75.00 0.425 1.3827 -0.3476 + 80.00 0.304 1.4202 -0.3625 + 85.00 0.179 1.4423 -0.3763 + 90.00 0.053 1.4512 -0.3890 + 95.00 -0.073 1.4480 -0.4004 + 100.00 -0.198 1.4294 -0.4105 + 105.00 -0.319 1.3954 -0.4191 + 110.00 -0.434 1.3464 -0.4260 + 115.00 -0.541 1.2829 -0.4308 + 120.00 -0.637 1.2057 -0.4333 + 125.00 -0.720 1.1157 -0.4330 + 130.00 -0.787 1.0144 -0.4294 + 135.00 -0.836 0.9033 -0.4219 + 140.00 -0.864 0.7845 -0.4098 + 145.00 -0.869 0.6605 -0.3922 + 150.00 -0.847 0.5346 -0.3682 + 155.00 -0.795 0.4103 -0.3364 + 160.00 -0.711 0.2922 -0.2954 + 170.00 -0.788 0.0969 -0.3966 + 175.00 -0.394 0.0334 -0.1978 + 180.00 0.000 0.0185 0.0000 diff --git a/examples/FAST.Farm_interface/inputs/FFFiles/Airfoils/DU21_A17_coords.txt b/examples/FAST.Farm_interface/inputs/FFFiles/Airfoils/DU21_A17_coords.txt new file mode 100644 index 00000000..72e36bf8 --- /dev/null +++ b/examples/FAST.Farm_interface/inputs/FFFiles/Airfoils/DU21_A17_coords.txt @@ -0,0 +1,407 @@ + 400 NumCoords ! The number of coordinates in the airfoil shape file (including an extra coordinate for airfoil reference). Set to zero if coordinates not included. +! ......... x-y coordinates are next if NumCoords > 0 ............. +! x-y coordinate of airfoil reference +! x/c y/c +0.25 0 +! coordinates of airfoil shape; data from TU Delft as posted here: https://wind.nrel.gov/forum/wind/viewtopic.php?f=2&t=440 +! DU 93-W-210.lm +! x/c y/c +1.00000 0.00194 +0.99660 0.00304 +0.99314 0.00411 +0.98961 0.00516 +0.98601 0.00618 +0.98235 0.00720 +0.97863 0.00823 +0.97484 0.00927 +0.97098 0.01033 +0.96706 0.01139 +0.96307 0.01246 +0.95902 0.01354 +0.95490 0.01463 +0.95072 0.01573 +0.94647 0.01684 +0.94216 0.01797 +0.93778 0.01911 +0.93333 0.02026 +0.92882 0.02142 +0.92425 0.02260 +0.91961 0.02379 +0.91490 0.02499 +0.91013 0.02621 +0.90529 0.02744 +0.90039 0.02869 +0.89542 0.02995 +0.89039 0.03122 +0.88529 0.03250 +0.88013 0.03379 +0.87490 0.03510 +0.86961 0.03643 +0.86425 0.03776 +0.85882 0.03912 +0.85333 0.04048 +0.84778 0.04186 +0.84216 0.04326 +0.83647 0.04466 +0.83072 0.04608 +0.82490 0.04752 +0.81902 0.04896 +0.81307 0.05041 +0.80706 0.05188 +0.80098 0.05336 +0.79484 0.05484 +0.78863 0.05634 +0.78235 0.05784 +0.77601 0.05936 +0.76961 0.06088 +0.76314 0.06242 +0.75660 0.06396 +0.75000 0.06550 +0.74333 0.06706 +0.73667 0.06860 +0.73000 0.07014 +0.72333 0.07167 +0.71667 0.07320 +0.71000 0.07472 +0.70333 0.07624 +0.69667 0.07774 +0.69000 0.07924 +0.68333 0.08072 +0.67667 0.08220 +0.67000 0.08366 +0.66333 0.08511 +0.65667 0.08655 +0.65000 0.08798 +0.64333 0.08940 +0.63667 0.09080 +0.63000 0.09220 +0.62333 0.09357 +0.61667 0.09492 +0.61000 0.09626 +0.60333 0.09759 +0.59667 0.09889 +0.59000 0.10017 +0.58333 0.10143 +0.57667 0.10267 +0.57000 0.10389 +0.56333 0.10509 +0.55667 0.10627 +0.55000 0.10742 +0.54333 0.10854 +0.53667 0.10964 +0.53000 0.11071 +0.52333 0.11175 +0.51667 0.11277 +0.51000 0.11375 +0.50333 0.11470 +0.49667 0.11562 +0.49000 0.11650 +0.48333 0.11734 +0.47667 0.11813 +0.47000 0.11889 +0.46333 0.11960 +0.45667 0.12027 +0.45000 0.12089 +0.44333 0.12147 +0.43667 0.12200 +0.43000 0.12249 +0.42333 0.12292 +0.41667 0.12331 +0.41000 0.12365 +0.40333 0.12394 +0.39667 0.12418 +0.39000 0.12436 +0.38333 0.12449 +0.37667 0.12457 +0.37000 0.12459 +0.36333 0.12455 +0.35667 0.12446 +0.35000 0.12431 +0.34333 0.12411 +0.33667 0.12385 +0.33000 0.12353 +0.32333 0.12317 +0.31667 0.12275 +0.31000 0.12228 +0.30333 0.12175 +0.29667 0.12117 +0.29000 0.12053 +0.28333 0.11984 +0.27667 0.11910 +0.27000 0.11829 +0.26333 0.11744 +0.25667 0.11653 +0.25000 0.11557 +0.24342 0.11456 +0.23693 0.11351 +0.23053 0.11243 +0.22421 0.11130 +0.21798 0.11015 +0.21184 0.10896 +0.20579 0.10773 +0.19982 0.10648 +0.19395 0.10520 +0.18816 0.10389 +0.18245 0.10255 +0.17684 0.10119 +0.17131 0.09980 +0.16587 0.09839 +0.16052 0.09696 +0.15526 0.09550 +0.15008 0.09403 +0.14499 0.09254 +0.13999 0.09103 +0.13508 0.08950 +0.13026 0.08796 +0.12552 0.08641 +0.12087 0.08483 +0.11631 0.08325 +0.11183 0.08165 +0.10745 0.08004 +0.10315 0.07843 +0.09893 0.07679 +0.09481 0.07516 +0.09077 0.07351 +0.08683 0.07186 +0.08297 0.07021 +0.07919 0.06854 +0.07551 0.06687 +0.07191 0.06520 +0.06840 0.06353 +0.06498 0.06185 +0.06164 0.06017 +0.05840 0.05850 +0.05524 0.05682 +0.05217 0.05515 +0.04918 0.05348 +0.04629 0.05181 +0.04348 0.05015 +0.04076 0.04849 +0.03812 0.04683 +0.03558 0.04519 +0.03312 0.04356 +0.03075 0.04194 +0.02847 0.04033 +0.02627 0.03874 +0.02417 0.03716 +0.02215 0.03560 +0.02022 0.03404 +0.01837 0.03249 +0.01662 0.03094 +0.01495 0.02940 +0.01337 0.02785 +0.01187 0.02630 +0.01047 0.02476 +0.00915 0.02322 +0.00792 0.02169 +0.00678 0.02017 +0.00572 0.01864 +0.00476 0.01713 +0.00388 0.01562 +0.00309 0.01410 +0.00238 0.01253 +0.00177 0.01094 +0.00124 0.00923 +0.00080 0.00740 +0.00044 0.00537 +0.00018 0.00333 +0.00000 0.00000 +0.00018 -0.00292 +0.00044 -0.00443 +0.00080 -0.00589 +0.00124 -0.00727 +0.00177 -0.00864 +0.00238 -0.00998 +0.00309 -0.01134 +0.00388 -0.01266 +0.00476 -0.01397 +0.00572 -0.01526 +0.00678 -0.01656 +0.00792 -0.01785 +0.00915 -0.01914 +0.01047 -0.02044 +0.01187 -0.02174 +0.01337 -0.02306 +0.01495 -0.02438 +0.01662 -0.02571 +0.01837 -0.02705 +0.02022 -0.02841 +0.02215 -0.02976 +0.02417 -0.03112 +0.02627 -0.03248 +0.02847 -0.03384 +0.03075 -0.03520 +0.03312 -0.03655 +0.03558 -0.03789 +0.03812 -0.03923 +0.04076 -0.04056 +0.04348 -0.04188 +0.04629 -0.04319 +0.04918 -0.04449 +0.05217 -0.04579 +0.05524 -0.04708 +0.05840 -0.04836 +0.06164 -0.04963 +0.06498 -0.05089 +0.06840 -0.05215 +0.07191 -0.05340 +0.07551 -0.05464 +0.07919 -0.05587 +0.08297 -0.05709 +0.08683 -0.05831 +0.09077 -0.05951 +0.09481 -0.06071 +0.09893 -0.06189 +0.10315 -0.06306 +0.10745 -0.06422 +0.11183 -0.06536 +0.11631 -0.06648 +0.12087 -0.06759 +0.12552 -0.06868 +0.13026 -0.06975 +0.13508 -0.07079 +0.13999 -0.07182 +0.14499 -0.07282 +0.15008 -0.07380 +0.15526 -0.07476 +0.16052 -0.07568 +0.16587 -0.07658 +0.17131 -0.07746 +0.17684 -0.07830 +0.18245 -0.07911 +0.18816 -0.07989 +0.19395 -0.08063 +0.19982 -0.08134 +0.20579 -0.08201 +0.21184 -0.08264 +0.21798 -0.08324 +0.22421 -0.08380 +0.23053 -0.08432 +0.23693 -0.08479 +0.24342 -0.08523 +0.25000 -0.08561 +0.25667 -0.08595 +0.26333 -0.08624 +0.27000 -0.08648 +0.27667 -0.08667 +0.28333 -0.08680 +0.29000 -0.08689 +0.29667 -0.08693 +0.30333 -0.08692 +0.31000 -0.08686 +0.31667 -0.08676 +0.32333 -0.08660 +0.33000 -0.08640 +0.33667 -0.08615 +0.34333 -0.08586 +0.35000 -0.08553 +0.35667 -0.08515 +0.36333 -0.08473 +0.37000 -0.08427 +0.37667 -0.08376 +0.38333 -0.08322 +0.39000 -0.08263 +0.39667 -0.08200 +0.40333 -0.08134 +0.41000 -0.08062 +0.41667 -0.07987 +0.42333 -0.07908 +0.43000 -0.07824 +0.43667 -0.07736 +0.44333 -0.07644 +0.45000 -0.07548 +0.45667 -0.07448 +0.46333 -0.07343 +0.47000 -0.07235 +0.47667 -0.07122 +0.48333 -0.07006 +0.49000 -0.06886 +0.49667 -0.06763 +0.50333 -0.06636 +0.51000 -0.06506 +0.51667 -0.06373 +0.52333 -0.06237 +0.53000 -0.06097 +0.53667 -0.05955 +0.54333 -0.05810 +0.55000 -0.05663 +0.55667 -0.05513 +0.56333 -0.05361 +0.57000 -0.05207 +0.57667 -0.05050 +0.58333 -0.04892 +0.59000 -0.04732 +0.59667 -0.04571 +0.60333 -0.04408 +0.61000 -0.04243 +0.61667 -0.04078 +0.62333 -0.03911 +0.63000 -0.03744 +0.63667 -0.03576 +0.64333 -0.03409 +0.65000 -0.03241 +0.65667 -0.03073 +0.66333 -0.02906 +0.67000 -0.02740 +0.67667 -0.02574 +0.68333 -0.02411 +0.69000 -0.02248 +0.69667 -0.02088 +0.70333 -0.01930 +0.71000 -0.01774 +0.71667 -0.01620 +0.72333 -0.01470 +0.73000 -0.01323 +0.73667 -0.01179 +0.74333 -0.01039 +0.75000 -0.00903 +0.75660 -0.00772 +0.76314 -0.00647 +0.76961 -0.00528 +0.77601 -0.00416 +0.78235 -0.00308 +0.78863 -0.00207 +0.79484 -0.00112 +0.80098 -0.00023 +0.80706 0.00060 +0.81307 0.00136 +0.81902 0.00207 +0.82490 0.00273 +0.83072 0.00333 +0.83647 0.00387 +0.84216 0.00435 +0.84778 0.00479 +0.85333 0.00517 +0.85882 0.00550 +0.86425 0.00578 +0.86961 0.00601 +0.87490 0.00620 +0.88013 0.00633 +0.88529 0.00643 +0.89039 0.00648 +0.89542 0.00649 +0.90039 0.00646 +0.90529 0.00639 +0.91013 0.00628 +0.91490 0.00613 +0.91961 0.00595 +0.92425 0.00574 +0.92882 0.00550 +0.93333 0.00523 +0.93778 0.00494 +0.94216 0.00462 +0.94647 0.00428 +0.95072 0.00392 +0.95490 0.00355 +0.95902 0.00315 +0.96307 0.00275 +0.96706 0.00233 +0.97098 0.00189 +0.97484 0.00145 +0.97863 0.00099 +0.98235 0.00053 +0.98601 0.00005 +0.98961 -0.00044 +0.99314 -0.00094 +0.99660 -0.00143 +1.00000 -0.00194 diff --git a/examples/FAST.Farm_interface/inputs/FFFiles/Airfoils/DU25_A17.dat b/examples/FAST.Farm_interface/inputs/FFFiles/Airfoils/DU25_A17.dat new file mode 100644 index 00000000..60730d0a --- /dev/null +++ b/examples/FAST.Farm_interface/inputs/FFFiles/Airfoils/DU25_A17.dat @@ -0,0 +1,194 @@ +! ------------ AirfoilInfo v1.01.x Input File ---------------------------------- +! DU25 airfoil with an aspect ratio of 17. Original -180 to 180deg Cl, Cd, and Cm versus AOA data taken from Appendix A of DOWEC document 10046_009.pdf (numerical values obtained from Koert Lindenburg of ECN). +! Cl and Cd values corrected for rotational stall delay and Cd values corrected using the Viterna method for 0 to 90deg AOA by Jason Jonkman using AirfoilPrep_v2p0.xls. +! note that this file uses Marshall Buhl's new input file processing; start all comment lines with ! +! ------------------------------------------------------------------------------ +"DEFAULT" InterpOrd ! Interpolation order to use for quasi-steady table lookup {1=linear; 3=cubic spline; "default"} [default=1] + 1 NonDimArea ! The non-dimensional area of the airfoil (area/chord^2) (set to 1.0 if unsure or unneeded) +@"DU25_A17_coords.txt" NumCoords ! The number of coordinates in the airfoil shape file. Set to zero if coordinates not included. +"unused" BL_file ! The file name including the boundary layer characteristics of the profile. Ignored if the aeroacoustic module is not called. + 1 NumTabs ! Number of airfoil tables in this file. +! ------------------------------------------------------------------------------ +! data for table 1 +! ------------------------------------------------------------------------------ + 0.75 Re ! Reynolds number in millions + 0 UserProp ! User property (control) setting +True InclUAdata ! Is unsteady aerodynamics data included in this table? If TRUE, then include 30 UA coefficients below this line +!........................................ + -3.2 alpha0 ! 0-lift angle of attack, depends on airfoil. + 8.5 alpha1 ! Angle of attack at f=0.7, (approximately the stall angle) for AOA>alpha0. (deg) + -8.5 alpha2 ! Angle of attack at f=0.7, (approximately the stall angle) for AOA1] + 0 S2 ! Constant in the f curve best-fit for AOA> alpha1; by definition it depends on the airfoil. [ignored if UAMod<>1] + 0 S3 ! Constant in the f curve best-fit for alpha2<=AOA< alpha0; by definition it depends on the airfoil. [ignored if UAMod<>1] + 0 S4 ! Constant in the f curve best-fit for AOA< alpha2; by definition it depends on the airfoil. [ignored if UAMod<>1] + 1.4336 Cn1 ! Critical value of C0n at leading edge separation. It should be extracted from airfoil data at a given Mach and Reynolds number. It can be calculated from the static value of Cn at either the break in the pitching moment or the loss of chord force at the onset of stall. It is close to the condition of maximum lift of the airfoil at low Mach numbers. + -0.6873 Cn2 ! As Cn1 for negative AOAs. + 0.19 St_sh ! Strouhal's shedding frequency constant. [default = 0.19] + 0.006 Cd0 ! 2D drag coefficient value at 0-lift. + -0.12 Cm0 ! 2D pitching moment coefficient about 1/4-chord location, at 0-lift, positive if nose up. [If the aerodynamics coefficients table does not include a column for Cm, this needs to be set to 0.0] + 0 k0 ! Constant in the \hat(x)_cp curve best-fit; = (\hat(x)_AC-0.25). [ignored if UAMod<>1] + 0 k1 ! Constant in the \hat(x)_cp curve best-fit. [ignored if UAMod<>1] + 0 k2 ! Constant in the \hat(x)_cp curve best-fit. [ignored if UAMod<>1] + 0 k3 ! Constant in the \hat(x)_cp curve best-fit. [ignored if UAMod<>1] + 0 k1_hat ! Constant in the expression of Cc due to leading edge vortex effects. [ignored if UAMod<>1] + 0.2 x_cp_bar ! Constant in the expression of \hat(x)_cp^v. [ignored if UAMod<>1, default = 0.2] +"DEFAULT" UACutout ! Angle of attack above which unsteady aerodynamics are disabled (deg). [Specifying the string "Default" sets UACutout to 45 degrees] +"DEFAULT" filtCutOff ! Reduced frequency cut-off for low-pass filtering the AoA input to UA, as well as the 1st and 2nd derivatives (-) [default = 0.5] +!........................................ +! Table of aerodynamics coefficients + 140 NumAlf ! Number of data lines in the following table +! Alpha Cl Cd Cm +! (deg) (-) (-) (-) + -180.00 0.000 0.0202 0.0000 + -175.00 0.368 0.0324 0.1845 + -170.00 0.735 0.0943 0.3701 + -160.00 0.695 0.2848 0.2679 + -155.00 0.777 0.4001 0.3046 + -150.00 0.828 0.5215 0.3329 + -145.00 0.850 0.6447 0.3540 + -140.00 0.846 0.7660 0.3693 + -135.00 0.818 0.8823 0.3794 + -130.00 0.771 0.9911 0.3854 + -125.00 0.705 1.0905 0.3878 + -120.00 0.624 1.1787 0.3872 + -115.00 0.530 1.2545 0.3841 + -110.00 0.426 1.3168 0.3788 + -105.00 0.314 1.3650 0.3716 + -100.00 0.195 1.3984 0.3629 + -95.00 0.073 1.4169 0.3529 + -90.00 -0.050 1.4201 0.3416 + -85.00 -0.173 1.4081 0.3292 + -80.00 -0.294 1.3811 0.3159 + -75.00 -0.409 1.3394 0.3017 + -70.00 -0.518 1.2833 0.2866 + -65.00 -0.617 1.2138 0.2707 + -60.00 -0.706 1.1315 0.2539 + -55.00 -0.780 1.0378 0.2364 + -50.00 -0.839 0.9341 0.2181 + -45.00 -0.879 0.8221 0.1991 + -40.00 -0.898 0.7042 0.1792 + -35.00 -0.893 0.5829 0.1587 + -30.00 -0.862 0.4616 0.1374 + -25.00 -0.803 0.3441 0.1154 + -24.00 -0.792 0.3209 0.1101 + -23.00 -0.789 0.2972 0.1031 + -22.00 -0.792 0.2730 0.0947 + -21.00 -0.801 0.2485 0.0849 + -20.00 -0.815 0.2237 0.0739 + -19.00 -0.833 0.1990 0.0618 + -18.00 -0.854 0.1743 0.0488 + -17.00 -0.879 0.1498 0.0351 + -16.00 -0.905 0.1256 0.0208 + -15.00 -0.932 0.1020 0.0060 + -14.00 -0.959 0.0789 -0.0091 + -13.00 -0.985 0.0567 -0.0243 + -12.01 -0.953 0.0271 -0.0349 + -11.00 -0.900 0.0303 -0.0361 + -9.98 -0.827 0.0287 -0.0464 + -8.98 -0.753 0.0271 -0.0534 + -8.47 -0.691 0.0264 -0.0650 + -7.45 -0.555 0.0114 -0.0782 + -6.42 -0.413 0.0094 -0.0904 + -5.40 -0.271 0.0086 -0.1006 + -5.00 -0.220 0.0073 -0.1107 + -4.50 -0.152 0.0071 -0.1135 + -4.00 -0.084 0.0070 -0.1162 + -3.50 -0.018 0.0069 -0.1186 + -3.00 0.049 0.0068 -0.1209 + -2.50 0.115 0.0068 -0.1231 + -2.00 0.181 0.0068 -0.1252 + -1.50 0.247 0.0067 -0.1272 + -1.00 0.312 0.0067 -0.1293 + -0.50 0.377 0.0067 -0.1311 + 0.00 0.444 0.0065 -0.1330 + 0.50 0.508 0.0065 -0.1347 + 1.00 0.573 0.0066 -0.1364 + 1.50 0.636 0.0067 -0.1380 + 2.00 0.701 0.0068 -0.1396 + 2.50 0.765 0.0069 -0.1411 + 3.00 0.827 0.0070 -0.1424 + 3.50 0.890 0.0071 -0.1437 + 4.00 0.952 0.0073 -0.1448 + 4.50 1.013 0.0076 -0.1456 + 5.00 1.062 0.0079 -0.1445 + 6.00 1.161 0.0099 -0.1419 + 6.50 1.208 0.0117 -0.1403 + 7.00 1.254 0.0132 -0.1382 + 7.50 1.301 0.0143 -0.1362 + 8.00 1.336 0.0153 -0.1320 + 8.50 1.369 0.0165 -0.1276 + 9.00 1.400 0.0181 -0.1234 + 9.50 1.428 0.0211 -0.1193 + 10.00 1.442 0.0262 -0.1152 + 10.50 1.427 0.0336 -0.1115 + 11.00 1.374 0.0420 -0.1081 + 11.50 1.316 0.0515 -0.1052 + 12.00 1.277 0.0601 -0.1026 + 12.50 1.250 0.0693 -0.1000 + 13.00 1.246 0.0785 -0.0980 + 13.50 1.247 0.0888 -0.0969 + 14.00 1.256 0.1000 -0.0968 + 14.50 1.260 0.1108 -0.0973 + 15.00 1.271 0.1219 -0.0981 + 15.50 1.281 0.1325 -0.0992 + 16.00 1.289 0.1433 -0.1006 + 16.50 1.294 0.1541 -0.1023 + 17.00 1.304 0.1649 -0.1042 + 17.50 1.309 0.1754 -0.1064 + 18.00 1.315 0.1845 -0.1082 + 18.50 1.320 0.1953 -0.1110 + 19.00 1.330 0.2061 -0.1143 + 19.50 1.343 0.2170 -0.1179 + 20.00 1.354 0.2280 -0.1219 + 20.50 1.359 0.2390 -0.1261 + 21.00 1.360 0.2536 -0.1303 + 22.00 1.325 0.2814 -0.1375 + 23.00 1.288 0.3098 -0.1446 + 24.00 1.251 0.3386 -0.1515 + 25.00 1.215 0.3678 -0.1584 + 26.00 1.181 0.3972 -0.1651 + 28.00 1.120 0.4563 -0.1781 + 30.00 1.076 0.5149 -0.1904 + 32.00 1.056 0.5720 -0.2017 + 35.00 1.066 0.6548 -0.2173 + 40.00 1.064 0.7901 -0.2418 + 45.00 1.035 0.9190 -0.2650 + 50.00 0.980 1.0378 -0.2867 + 55.00 0.904 1.1434 -0.3072 + 60.00 0.810 1.2333 -0.3265 + 65.00 0.702 1.3055 -0.3446 + 70.00 0.582 1.3587 -0.3616 + 75.00 0.456 1.3922 -0.3775 + 80.00 0.326 1.4063 -0.3921 + 85.00 0.197 1.4042 -0.4057 + 90.00 0.072 1.3985 -0.4180 + 95.00 -0.050 1.3973 -0.4289 + 100.00 -0.170 1.3810 -0.4385 + 105.00 -0.287 1.3498 -0.4464 + 110.00 -0.399 1.3041 -0.4524 + 115.00 -0.502 1.2442 -0.4563 + 120.00 -0.596 1.1709 -0.4577 + 125.00 -0.677 1.0852 -0.4563 + 130.00 -0.743 0.9883 -0.4514 + 135.00 -0.792 0.8818 -0.4425 + 140.00 -0.821 0.7676 -0.4288 + 145.00 -0.826 0.6481 -0.4095 + 150.00 -0.806 0.5264 -0.3836 + 155.00 -0.758 0.4060 -0.3497 + 160.00 -0.679 0.2912 -0.3065 + 170.00 -0.735 0.0995 -0.3706 + 175.00 -0.368 0.0356 -0.1846 + 180.00 0.000 0.0202 0.0000 diff --git a/examples/FAST.Farm_interface/inputs/FFFiles/Airfoils/DU25_A17_coords.txt b/examples/FAST.Farm_interface/inputs/FFFiles/Airfoils/DU25_A17_coords.txt new file mode 100644 index 00000000..8e481fb8 --- /dev/null +++ b/examples/FAST.Farm_interface/inputs/FFFiles/Airfoils/DU25_A17_coords.txt @@ -0,0 +1,407 @@ + 400 NumCoords ! The number of coordinates in the airfoil shape file (including an extra coordinate for airfoil reference). Set to zero if coordinates not included. +! ......... x-y coordinates are next if NumCoords > 0 ............. +! x-y coordinate of airfoil reference +! x/c y/c +0.25 0 +! coordinates of airfoil shape; data from TU Delft as posted here: https://wind.nrel.gov/forum/wind/viewtopic.php?f=2&t=440 +! DU 91-W2-250.lm +! x/c y/c +1.00000 0.00213 +0.99660 0.00314 +0.99314 0.00414 +0.98961 0.00515 +0.98601 0.00617 +0.98235 0.00720 +0.97863 0.00822 +0.97484 0.00926 +0.97098 0.01030 +0.96706 0.01135 +0.96307 0.01240 +0.95902 0.01347 +0.95490 0.01454 +0.95072 0.01562 +0.94647 0.01672 +0.94216 0.01783 +0.93778 0.01895 +0.93333 0.02009 +0.92882 0.02125 +0.92425 0.02241 +0.91961 0.02359 +0.91490 0.02479 +0.91013 0.02600 +0.90529 0.02722 +0.90039 0.02846 +0.89542 0.02972 +0.89039 0.03099 +0.88529 0.03227 +0.88013 0.03357 +0.87490 0.03489 +0.86961 0.03622 +0.86425 0.03756 +0.85882 0.03892 +0.85333 0.04029 +0.84778 0.04167 +0.84216 0.04306 +0.83647 0.04447 +0.83072 0.04589 +0.82490 0.04732 +0.81902 0.04877 +0.81307 0.05023 +0.80706 0.05170 +0.80098 0.05319 +0.79484 0.05468 +0.78863 0.05619 +0.78235 0.05771 +0.77601 0.05925 +0.76961 0.06078 +0.76314 0.06233 +0.75660 0.06388 +0.75000 0.06544 +0.74333 0.06701 +0.73667 0.06857 +0.73000 0.07013 +0.72333 0.07168 +0.71667 0.07322 +0.71000 0.07475 +0.70333 0.07628 +0.69667 0.07779 +0.69000 0.07930 +0.68333 0.08080 +0.67667 0.08228 +0.67000 0.08375 +0.66333 0.08522 +0.65667 0.08667 +0.65000 0.08810 +0.64333 0.08953 +0.63667 0.09093 +0.63000 0.09233 +0.62333 0.09371 +0.61667 0.09507 +0.61000 0.09642 +0.60333 0.09775 +0.59667 0.09906 +0.59000 0.10035 +0.58333 0.10163 +0.57667 0.10289 +0.57000 0.10413 +0.56333 0.10535 +0.55667 0.10655 +0.55000 0.10773 +0.54333 0.10888 +0.53667 0.11001 +0.53000 0.11112 +0.52333 0.11221 +0.51667 0.11327 +0.51000 0.11430 +0.50333 0.11530 +0.49667 0.11628 +0.49000 0.11723 +0.48333 0.11815 +0.47667 0.11904 +0.47000 0.11991 +0.46333 0.12074 +0.45667 0.12154 +0.45000 0.12230 +0.44333 0.12303 +0.43667 0.12372 +0.43000 0.12436 +0.42333 0.12497 +0.41667 0.12554 +0.41000 0.12606 +0.40333 0.12655 +0.39667 0.12699 +0.39000 0.12738 +0.38333 0.12773 +0.37667 0.12803 +0.37000 0.12828 +0.36333 0.12846 +0.35667 0.12858 +0.35000 0.12864 +0.34333 0.12862 +0.33667 0.12853 +0.33000 0.12837 +0.32333 0.12815 +0.31667 0.12785 +0.31000 0.12749 +0.30333 0.12705 +0.29667 0.12656 +0.29000 0.12600 +0.28333 0.12538 +0.27667 0.12469 +0.27000 0.12394 +0.26333 0.12312 +0.25667 0.12224 +0.25000 0.12130 +0.24342 0.12030 +0.23693 0.11926 +0.23053 0.11817 +0.22421 0.11704 +0.21798 0.11586 +0.21184 0.11465 +0.20579 0.11340 +0.19982 0.11210 +0.19395 0.11078 +0.18816 0.10942 +0.18245 0.10803 +0.17684 0.10660 +0.17131 0.10515 +0.16587 0.10367 +0.16052 0.10217 +0.15526 0.10064 +0.15008 0.09909 +0.14499 0.09751 +0.13999 0.09591 +0.13508 0.09430 +0.13026 0.09266 +0.12552 0.09101 +0.12087 0.08934 +0.11631 0.08765 +0.11183 0.08595 +0.10745 0.08424 +0.10315 0.08251 +0.09893 0.08076 +0.09481 0.07902 +0.09077 0.07725 +0.08683 0.07549 +0.08297 0.07371 +0.07919 0.07192 +0.07551 0.07013 +0.07191 0.06834 +0.06840 0.06654 +0.06498 0.06474 +0.06164 0.06293 +0.05840 0.06113 +0.05524 0.05933 +0.05217 0.05753 +0.04918 0.05573 +0.04629 0.05393 +0.04348 0.05214 +0.04076 0.05035 +0.03812 0.04856 +0.03558 0.04679 +0.03312 0.04502 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+0.71000 -0.02456 +0.71667 -0.02238 +0.72333 -0.02026 +0.73000 -0.01817 +0.73667 -0.01614 +0.74333 -0.01416 +0.75000 -0.01223 +0.75660 -0.01038 +0.76314 -0.00861 +0.76961 -0.00692 +0.77601 -0.00532 +0.78235 -0.00381 +0.78863 -0.00238 +0.79484 -0.00103 +0.80098 0.00023 +0.80706 0.00141 +0.81307 0.00250 +0.81902 0.00351 +0.82490 0.00444 +0.83072 0.00529 +0.83647 0.00606 +0.84216 0.00675 +0.84778 0.00737 +0.85333 0.00791 +0.85882 0.00839 +0.86425 0.00879 +0.86961 0.00913 +0.87490 0.00940 +0.88013 0.00961 +0.88529 0.00975 +0.89039 0.00983 +0.89542 0.00985 +0.90039 0.00982 +0.90529 0.00972 +0.91013 0.00957 +0.91490 0.00936 +0.91961 0.00910 +0.92425 0.00880 +0.92882 0.00844 +0.93333 0.00804 +0.93778 0.00760 +0.94216 0.00712 +0.94647 0.00660 +0.95072 0.00606 +0.95490 0.00549 +0.95902 0.00490 +0.96307 0.00429 +0.96706 0.00367 +0.97098 0.00303 +0.97484 0.00238 +0.97863 0.00173 +0.98235 0.00108 +0.98601 0.00043 +0.98961 -0.00022 +0.99314 -0.00086 +0.99660 -0.00149 +1.00000 -0.00213 diff --git a/examples/FAST.Farm_interface/inputs/FFFiles/Airfoils/DU30_A17.dat b/examples/FAST.Farm_interface/inputs/FFFiles/Airfoils/DU30_A17.dat new file mode 100644 index 00000000..438015cb --- /dev/null +++ b/examples/FAST.Farm_interface/inputs/FFFiles/Airfoils/DU30_A17.dat @@ -0,0 +1,198 @@ +! ------------ AirfoilInfo v1.01.x Input File ---------------------------------- +! DU30 airfoil with an aspect ratio of 17. Original -180 to 180deg Cl, Cd, and Cm versus AOA data taken from Appendix A of DOWEC document 10046_009.pdf (numerical values obtained from Koert Lindenburg of ECN). +! Cl and Cd values corrected for rotational stall delay and Cd values corrected using the Viterna method for 0 to 90deg AOA by Jason Jonkman using AirfoilPrep_v2p0.xls. +! note that this file uses Marshall Buhl's new input file processing; start all comment lines with ! +! ------------------------------------------------------------------------------ +"DEFAULT" InterpOrd ! Interpolation order to use for quasi-steady table lookup {1=linear; 3=cubic spline; "default"} [default=1] + 1 NonDimArea ! The non-dimensional area of the airfoil (area/chord^2) (set to 1.0 if unsure or unneeded) +@"DU30_A17_coords.txt" NumCoords ! The number of coordinates in the airfoil shape file. Set to zero if coordinates not included. +"unused" BL_file ! The file name including the boundary layer characteristics of the profile. Ignored if the aeroacoustic module is not called. + 1 NumTabs ! Number of airfoil tables in this file. +! ------------------------------------------------------------------------------ +! data for table 1 +! ------------------------------------------------------------------------------ + 0.75 Re ! Reynolds number in millions + 0 UserProp ! User property (control) setting +True InclUAdata ! Is unsteady aerodynamics data included in this table? If TRUE, then include 30 UA coefficients below this line +!........................................ + -2.2 alpha0 ! 0-lift angle of attack, depends on airfoil. + 9 alpha1 ! Angle of attack at f=0.7, (approximately the stall angle) for AOA>alpha0. (deg) + -9 alpha2 ! Angle of attack at f=0.7, (approximately the stall angle) for AOA1] + 0 S2 ! Constant in the f curve best-fit for AOA> alpha1; by definition it depends on the airfoil. [ignored if UAMod<>1] + 0 S3 ! Constant in the f curve best-fit for alpha2<=AOA< alpha0; by definition it depends on the airfoil. [ignored if UAMod<>1] + 0 S4 ! Constant in the f curve best-fit for AOA< alpha2; by definition it depends on the airfoil. [ignored if UAMod<>1] + 1.449 Cn1 ! Critical value of C0n at leading edge separation. It should be extracted from airfoil data at a given Mach and Reynolds number. It can be calculated from the static value of Cn at either the break in the pitching moment or the loss of chord force at the onset of stall. It is close to the condition of maximum lift of the airfoil at low Mach numbers. + -0.6138 Cn2 ! As Cn1 for negative AOAs. + 0.19 St_sh ! Strouhal's shedding frequency constant. [default = 0.19] + 0.008 Cd0 ! 2D drag coefficient value at 0-lift. + -0.09 Cm0 ! 2D pitching moment coefficient about 1/4-chord location, at 0-lift, positive if nose up. [If the aerodynamics coefficients table does not include a column for Cm, this needs to be set to 0.0] + 0 k0 ! Constant in the \hat(x)_cp curve best-fit; = (\hat(x)_AC-0.25). [ignored if UAMod<>1] + 0 k1 ! Constant in the \hat(x)_cp curve best-fit. [ignored if UAMod<>1] + 0 k2 ! Constant in the \hat(x)_cp curve best-fit. [ignored if UAMod<>1] + 0 k3 ! Constant in the \hat(x)_cp curve best-fit. [ignored if UAMod<>1] + 0 k1_hat ! Constant in the expression of Cc due to leading edge vortex effects. [ignored if UAMod<>1] + 0.2 x_cp_bar ! Constant in the expression of \hat(x)_cp^v. [ignored if UAMod<>1, default = 0.2] +"DEFAULT" UACutout ! Angle of attack above which unsteady aerodynamics are disabled (deg). [Specifying the string "Default" sets UACutout to 45 degrees] +"DEFAULT" filtCutOff ! Reduced frequency cut-off for low-pass filtering the AoA input to UA, as well as the 1st and 2nd derivatives (-) [default = 0.5] +!........................................ +! Table of aerodynamics coefficients + 143 NumAlf ! Number of data lines in the following table +! Alpha Cl Cd Cm +! (deg) (-) (-) (-) + -180.00 0.000 0.0267 0.0000 + -175.00 0.274 0.0370 0.1379 + -170.00 0.547 0.0968 0.2778 + -160.00 0.685 0.2876 0.2740 + -155.00 0.766 0.4025 0.3118 + -150.00 0.816 0.5232 0.3411 + -145.00 0.836 0.6454 0.3631 + -140.00 0.832 0.7656 0.3791 + -135.00 0.804 0.8807 0.3899 + -130.00 0.756 0.9882 0.3965 + -125.00 0.690 1.0861 0.3994 + -120.00 0.609 1.1730 0.3992 + -115.00 0.515 1.2474 0.3964 + -110.00 0.411 1.3084 0.3915 + -105.00 0.300 1.3552 0.3846 + -100.00 0.182 1.3875 0.3761 + -95.00 0.061 1.4048 0.3663 + -90.00 -0.061 1.4070 0.3551 + -85.00 -0.183 1.3941 0.3428 + -80.00 -0.302 1.3664 0.3295 + -75.00 -0.416 1.3240 0.3153 + -70.00 -0.523 1.2676 0.3001 + -65.00 -0.622 1.1978 0.2841 + -60.00 -0.708 1.1156 0.2672 + -55.00 -0.781 1.0220 0.2494 + -50.00 -0.838 0.9187 0.2308 + -45.00 -0.877 0.8074 0.2113 + -40.00 -0.895 0.6904 0.1909 + -35.00 -0.889 0.5703 0.1696 + -30.00 -0.858 0.4503 0.1475 + -25.00 -0.832 0.3357 0.1224 + -24.00 -0.852 0.3147 0.1156 + -23.00 -0.882 0.2946 0.1081 + -22.00 -0.919 0.2752 0.1000 + -21.00 -0.963 0.2566 0.0914 + -20.00 -1.013 0.2388 0.0823 + -19.00 -1.067 0.2218 0.0728 + -18.00 -1.125 0.2056 0.0631 + -17.00 -1.185 0.1901 0.0531 + -16.00 -1.245 0.1754 0.0430 + -15.25 -1.290 0.1649 0.0353 + -14.24 -1.229 0.1461 0.0240 + -13.24 -1.148 0.1263 0.0100 + -12.22 -1.052 0.1051 -0.0090 + -11.22 -0.965 0.0886 -0.0230 + -10.19 -0.867 0.0740 -0.0336 + -9.70 -0.822 0.0684 -0.0375 + -9.18 -0.769 0.0605 -0.0440 + -8.18 -0.756 0.0270 -0.0578 + -7.19 -0.690 0.0180 -0.0590 + -6.65 -0.616 0.0166 -0.0633 + -6.13 -0.542 0.0152 -0.0674 + -6.00 -0.525 0.0117 -0.0732 + -5.50 -0.451 0.0105 -0.0766 + -5.00 -0.382 0.0097 -0.0797 + -4.50 -0.314 0.0092 -0.0825 + -4.00 -0.251 0.0091 -0.0853 + -3.50 -0.189 0.0089 -0.0884 + -3.00 -0.120 0.0089 -0.0914 + -2.50 -0.051 0.0088 -0.0942 + -2.00 0.017 0.0088 -0.0969 + -1.50 0.085 0.0088 -0.0994 + -1.00 0.152 0.0088 -0.1018 + -0.50 0.219 0.0088 -0.1041 + 0.00 0.288 0.0087 -0.1062 + 0.50 0.354 0.0087 -0.1086 + 1.00 0.421 0.0088 -0.1107 + 1.50 0.487 0.0089 -0.1129 + 2.00 0.554 0.0090 -0.1149 + 2.50 0.619 0.0091 -0.1168 + 3.00 0.685 0.0092 -0.1185 + 3.50 0.749 0.0093 -0.1201 + 4.00 0.815 0.0095 -0.1218 + 4.50 0.879 0.0096 -0.1233 + 5.00 0.944 0.0097 -0.1248 + 5.50 1.008 0.0099 -0.1260 + 6.00 1.072 0.0101 -0.1270 + 6.50 1.135 0.0103 -0.1280 + 7.00 1.197 0.0107 -0.1287 + 7.50 1.256 0.0112 -0.1289 + 8.00 1.305 0.0125 -0.1270 + 9.00 1.390 0.0155 -0.1207 + 9.50 1.424 0.0171 -0.1158 + 10.00 1.458 0.0192 -0.1116 + 10.50 1.488 0.0219 -0.1073 + 11.00 1.512 0.0255 -0.1029 + 11.50 1.533 0.0307 -0.0983 + 12.00 1.549 0.0370 -0.0949 + 12.50 1.558 0.0452 -0.0921 + 13.00 1.470 0.0630 -0.0899 + 13.50 1.398 0.0784 -0.0885 + 14.00 1.354 0.0931 -0.0885 + 14.50 1.336 0.1081 -0.0902 + 15.00 1.333 0.1239 -0.0928 + 15.50 1.326 0.1415 -0.0963 + 16.00 1.329 0.1592 -0.1006 + 16.50 1.326 0.1743 -0.1042 + 17.00 1.321 0.1903 -0.1084 + 17.50 1.331 0.2044 -0.1125 + 18.00 1.333 0.2186 -0.1169 + 18.50 1.340 0.2324 -0.1215 + 19.00 1.362 0.2455 -0.1263 + 19.50 1.382 0.2584 -0.1313 + 20.00 1.398 0.2689 -0.1352 + 20.50 1.426 0.2814 -0.1406 + 21.00 1.437 0.2943 -0.1462 + 22.00 1.418 0.3246 -0.1516 + 23.00 1.397 0.3557 -0.1570 + 24.00 1.376 0.3875 -0.1623 + 25.00 1.354 0.4198 -0.1676 + 26.00 1.332 0.4524 -0.1728 + 28.00 1.293 0.5183 -0.1832 + 30.00 1.265 0.5843 -0.1935 + 32.00 1.253 0.6492 -0.2039 + 35.00 1.264 0.7438 -0.2193 + 40.00 1.258 0.8970 -0.2440 + 45.00 1.217 1.0402 -0.2672 + 50.00 1.146 1.1686 -0.2891 + 55.00 1.049 1.2779 -0.3097 + 60.00 0.932 1.3647 -0.3290 + 65.00 0.799 1.4267 -0.3471 + 70.00 0.657 1.4621 -0.3641 + 75.00 0.509 1.4708 -0.3799 + 80.00 0.362 1.4544 -0.3946 + 85.00 0.221 1.4196 -0.4081 + 90.00 0.092 1.3938 -0.4204 + 95.00 -0.030 1.3943 -0.4313 + 100.00 -0.150 1.3798 -0.4408 + 105.00 -0.267 1.3504 -0.4486 + 110.00 -0.379 1.3063 -0.4546 + 115.00 -0.483 1.2481 -0.4584 + 120.00 -0.578 1.1763 -0.4597 + 125.00 -0.660 1.0919 -0.4582 + 130.00 -0.727 0.9962 -0.4532 + 135.00 -0.777 0.8906 -0.4441 + 140.00 -0.807 0.7771 -0.4303 + 145.00 -0.815 0.6581 -0.4109 + 150.00 -0.797 0.5364 -0.3848 + 155.00 -0.750 0.4157 -0.3508 + 160.00 -0.673 0.3000 -0.3074 + 170.00 -0.547 0.1051 -0.2786 + 175.00 -0.274 0.0388 -0.1380 + 180.00 0.000 0.0267 0.0000 + diff --git a/examples/FAST.Farm_interface/inputs/FFFiles/Airfoils/DU30_A17_coords.txt b/examples/FAST.Farm_interface/inputs/FFFiles/Airfoils/DU30_A17_coords.txt new file mode 100644 index 00000000..722bf83a --- /dev/null +++ b/examples/FAST.Farm_interface/inputs/FFFiles/Airfoils/DU30_A17_coords.txt @@ -0,0 +1,407 @@ + 400 NumCoords ! The number of coordinates in the airfoil shape file (including an extra coordinate for airfoil reference). Set to zero if coordinates not included. +! ......... x-y coordinates are next if NumCoords > 0 ............. +! x-y coordinate of airfoil reference +! x/c y/c +0.25 0 +! coordinates of airfoil shape; data from TU Delft as posted here: https://wind.nrel.gov/forum/wind/viewtopic.php?f=2&t=440 +! DU 97-W-300.lm +! x/c y/c +1.00000 0.00246 +0.99660 0.00340 +0.99314 0.00437 +0.98961 0.00536 +0.98601 0.00638 +0.98235 0.00740 +0.97863 0.00843 +0.97484 0.00947 +0.97098 0.01051 +0.96706 0.01157 +0.96307 0.01264 +0.95902 0.01371 +0.95490 0.01479 +0.95072 0.01588 +0.94647 0.01698 +0.94216 0.01810 +0.93778 0.01922 +0.93333 0.02036 +0.92882 0.02151 +0.92425 0.02268 +0.91961 0.02386 +0.91490 0.02505 +0.91013 0.02626 +0.90529 0.02749 +0.90039 0.02873 +0.89542 0.02999 +0.89039 0.03126 +0.88529 0.03255 +0.88013 0.03385 +0.87490 0.03516 +0.86961 0.03649 +0.86425 0.03784 +0.85882 0.03921 +0.85333 0.04058 +0.84778 0.04197 +0.84216 0.04337 +0.83647 0.04479 +0.83072 0.04622 +0.82490 0.04767 +0.81902 0.04913 +0.81307 0.05060 +0.80706 0.05208 +0.80098 0.05357 +0.79484 0.05508 +0.78863 0.05659 +0.78235 0.05812 +0.77601 0.05965 +0.76961 0.06120 +0.76314 0.06275 +0.75660 0.06432 +0.75000 0.06589 +0.74333 0.06747 +0.73667 0.06904 +0.73000 0.07061 +0.72333 0.07217 +0.71667 0.07371 +0.71000 0.07525 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0.13420 +0.31000 0.13424 +0.30333 0.13422 +0.29667 0.13415 +0.29000 0.13401 +0.28333 0.13381 +0.27667 0.13355 +0.27000 0.13321 +0.26333 0.13280 +0.25667 0.13231 +0.25000 0.13174 +0.24342 0.13109 +0.23693 0.13036 +0.23053 0.12955 +0.22421 0.12866 +0.21798 0.12771 +0.21184 0.12668 +0.20579 0.12559 +0.19982 0.12444 +0.19395 0.12324 +0.18816 0.12197 +0.18245 0.12066 +0.17684 0.11930 +0.17131 0.11789 +0.16587 0.11644 +0.16052 0.11495 +0.15526 0.11342 +0.15008 0.11185 +0.14499 0.11024 +0.13999 0.10860 +0.13508 0.10693 +0.13026 0.10522 +0.12552 0.10348 +0.12087 0.10172 +0.11631 0.09993 +0.11183 0.09811 +0.10745 0.09627 +0.10315 0.09441 +0.09893 0.09252 +0.09481 0.09061 +0.09077 0.08869 +0.08683 0.08675 +0.08297 0.08478 +0.07919 0.08280 +0.07551 0.08082 +0.07191 0.07881 +0.06840 0.07680 +0.06498 0.07477 +0.06164 0.07274 +0.05840 0.07070 +0.05524 0.06865 +0.05217 0.06660 +0.04918 0.06454 +0.04629 0.06248 +0.04348 0.06042 +0.04076 0.05835 +0.03812 0.05629 +0.03558 0.05423 +0.03312 0.05217 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--git a/examples/FAST.Farm_interface/inputs/FFFiles/Airfoils/DU35_A17.dat b/examples/FAST.Farm_interface/inputs/FFFiles/Airfoils/DU35_A17.dat new file mode 100644 index 00000000..48e2b5f3 --- /dev/null +++ b/examples/FAST.Farm_interface/inputs/FFFiles/Airfoils/DU35_A17.dat @@ -0,0 +1,189 @@ +! ------------ AirfoilInfo v1.01.x Input File ---------------------------------- +! DU35 airfoil with an aspect ratio of 17. Original -180 to 180deg Cl, Cd, and Cm versus AOA data taken from Appendix A of DOWEC document 10046_009.pdf (numerical values obtained from Koert Lindenburg of ECN). +! Cl and Cd values corrected for rotational stall delay and Cd values corrected using the Viterna method for 0 to 90deg AOA by Jason Jonkman using AirfoilPrep_v2p0.xls. +! note that this file uses Marshall Buhl's new input file processing; start all comment lines with ! +! ------------------------------------------------------------------------------ +"DEFAULT" InterpOrd ! Interpolation order to use for quasi-steady table lookup {1=linear; 3=cubic spline; "default"} [default=1] + 1 NonDimArea ! The non-dimensional area of the airfoil (area/chord^2) (set to 1.0 if unsure or unneeded) +@"DU35_A17_coords.txt" NumCoords ! The number of coordinates in the airfoil shape file. Set to zero if coordinates not included. +"unused" BL_file ! The file name including the boundary layer characteristics of the profile. Ignored if the aeroacoustic module is not called. + 1 NumTabs ! Number of airfoil tables in this file. +! ------------------------------------------------------------------------------ +! data for table 1 +! ------------------------------------------------------------------------------ + 0.75 Re ! Reynolds number in millions + 0 UserProp ! User property (control) setting +True InclUAdata ! Is unsteady aerodynamics data included in this table? If TRUE, then include 30 UA coefficients below this line +!........................................ + -1.2 alpha0 ! 0-lift angle of attack, depends on airfoil. + 11.5 alpha1 ! Angle of attack at f=0.7, (approximately the stall angle) for AOA>alpha0. (deg) + -11.5 alpha2 ! Angle of attack at f=0.7, (approximately the stall angle) for AOA1] + 0 S2 ! Constant in the f curve best-fit for AOA> alpha1; by definition it depends on the airfoil. [ignored if UAMod<>1] + 0 S3 ! Constant in the f curve best-fit for alpha2<=AOA< alpha0; by definition it depends on the airfoil. [ignored if UAMod<>1] + 0 S4 ! Constant in the f curve best-fit for AOA< alpha2; by definition it depends on the airfoil. [ignored if UAMod<>1] + 1.6717 Cn1 ! Critical value of C0n at leading edge separation. It should be extracted from airfoil data at a given Mach and Reynolds number. It can be calculated from the static value of Cn at either the break in the pitching moment or the loss of chord force at the onset of stall. It is close to the condition of maximum lift of the airfoil at low Mach numbers. + -0.3075 Cn2 ! As Cn1 for negative AOAs. + 0.19 St_sh ! Strouhal's shedding frequency constant. [default = 0.19] + 0.012 Cd0 ! 2D drag coefficient value at 0-lift. + -0.07 Cm0 ! 2D pitching moment coefficient about 1/4-chord location, at 0-lift, positive if nose up. [If the aerodynamics coefficients table does not include a column for Cm, this needs to be set to 0.0] + 0 k0 ! Constant in the \hat(x)_cp curve best-fit; = (\hat(x)_AC-0.25). [ignored if UAMod<>1] + 0 k1 ! Constant in the \hat(x)_cp curve best-fit. [ignored if UAMod<>1] + 0 k2 ! Constant in the \hat(x)_cp curve best-fit. [ignored if UAMod<>1] + 0 k3 ! Constant in the \hat(x)_cp curve best-fit. [ignored if UAMod<>1] + 0 k1_hat ! Constant in the expression of Cc due to leading edge vortex effects. [ignored if UAMod<>1] + 0.2 x_cp_bar ! Constant in the expression of \hat(x)_cp^v. [ignored if UAMod<>1, default = 0.2] +"DEFAULT" UACutout ! Angle of attack above which unsteady aerodynamics are disabled (deg). [Specifying the string "Default" sets UACutout to 45 degrees] +"DEFAULT" filtCutOff ! Reduced frequency cut-off for low-pass filtering the AoA input to UA, as well as the 1st and 2nd derivatives (-) [default = 0.5] +!........................................ +! Table of aerodynamics coefficients + 135 NumAlf ! Number of data lines in the following table +! Alpha Cl Cd Cm +! (deg) (-) (-) (-) + -180.00 0.000 0.0407 0.0000 + -175.00 0.223 0.0507 0.0937 + -170.00 0.405 0.1055 0.1702 + -160.00 0.658 0.2982 0.2819 + -155.00 0.733 0.4121 0.3213 + -150.00 0.778 0.5308 0.3520 + -145.00 0.795 0.6503 0.3754 + -140.00 0.787 0.7672 0.3926 + -135.00 0.757 0.8785 0.4046 + -130.00 0.708 0.9819 0.4121 + -125.00 0.641 1.0756 0.4160 + -120.00 0.560 1.1580 0.4167 + -115.00 0.467 1.2280 0.4146 + -110.00 0.365 1.2847 0.4104 + -105.00 0.255 1.3274 0.4041 + -100.00 0.139 1.3557 0.3961 + -95.00 0.021 1.3692 0.3867 + -90.00 -0.098 1.3680 0.3759 + -85.00 -0.216 1.3521 0.3639 + -80.00 -0.331 1.3218 0.3508 + -75.00 -0.441 1.2773 0.3367 + -70.00 -0.544 1.2193 0.3216 + -65.00 -0.638 1.1486 0.3054 + -60.00 -0.720 1.0660 0.2884 + -55.00 -0.788 0.9728 0.2703 + -50.00 -0.840 0.8705 0.2512 + -45.00 -0.875 0.7611 0.2311 + -40.00 -0.889 0.6466 0.2099 + -35.00 -0.880 0.5299 0.1876 + -30.00 -0.846 0.4141 0.1641 + -25.00 -0.784 0.3030 0.1396 + -24.00 -0.768 0.2817 0.1345 + -23.00 -0.751 0.2608 0.1294 + -22.00 -0.733 0.2404 0.1243 + -21.00 -0.714 0.2205 0.1191 + -20.00 -0.693 0.2011 0.1139 + -19.00 -0.671 0.1822 0.1086 + -18.00 -0.648 0.1640 0.1032 + -17.00 -0.624 0.1465 0.0975 + -16.00 -0.601 0.1300 0.0898 + -15.00 -0.579 0.1145 0.0799 + -14.00 -0.559 0.1000 0.0682 + -13.00 -0.539 0.0867 0.0547 + -12.00 -0.519 0.0744 0.0397 + -11.00 -0.499 0.0633 0.0234 + -10.00 -0.480 0.0534 0.0060 + -5.54 -0.385 0.0245 -0.0800 + -5.04 -0.359 0.0225 -0.0800 + -4.54 -0.360 0.0196 -0.0800 + -4.04 -0.355 0.0174 -0.0800 + -3.54 -0.307 0.0162 -0.0800 + -3.04 -0.246 0.0144 -0.0800 + -3.00 -0.240 0.0240 -0.0623 + -2.50 -0.163 0.0188 -0.0674 + -2.00 -0.091 0.0160 -0.0712 + -1.50 -0.019 0.0137 -0.0746 + -1.00 0.052 0.0118 -0.0778 + -0.50 0.121 0.0104 -0.0806 + 0.00 0.196 0.0094 -0.0831 + 0.50 0.265 0.0096 -0.0863 + 1.00 0.335 0.0098 -0.0895 + 1.50 0.404 0.0099 -0.0924 + 2.00 0.472 0.0100 -0.0949 + 2.50 0.540 0.0102 -0.0973 + 3.00 0.608 0.0103 -0.0996 + 3.50 0.674 0.0104 -0.1016 + 4.00 0.742 0.0105 -0.1037 + 4.50 0.809 0.0107 -0.1057 + 5.00 0.875 0.0108 -0.1076 + 5.50 0.941 0.0109 -0.1094 + 6.00 1.007 0.0110 -0.1109 + 6.50 1.071 0.0113 -0.1118 + 7.00 1.134 0.0115 -0.1127 + 7.50 1.198 0.0117 -0.1138 + 8.00 1.260 0.0120 -0.1144 + 8.50 1.318 0.0126 -0.1137 + 9.00 1.368 0.0133 -0.1112 + 9.50 1.422 0.0143 -0.1100 + 10.00 1.475 0.0156 -0.1086 + 10.50 1.523 0.0174 -0.1064 + 11.00 1.570 0.0194 -0.1044 + 11.50 1.609 0.0227 -0.1013 + 12.00 1.642 0.0269 -0.0980 + 12.50 1.675 0.0319 -0.0953 + 13.00 1.700 0.0398 -0.0925 + 13.50 1.717 0.0488 -0.0896 + 14.00 1.712 0.0614 -0.0864 + 14.50 1.703 0.0786 -0.0840 + 15.50 1.671 0.1173 -0.0830 + 16.00 1.649 0.1377 -0.0848 + 16.50 1.621 0.1600 -0.0880 + 17.00 1.598 0.1814 -0.0926 + 17.50 1.571 0.2042 -0.0984 + 18.00 1.549 0.2316 -0.1052 + 19.00 1.544 0.2719 -0.1158 + 19.50 1.549 0.2906 -0.1213 + 20.00 1.565 0.3085 -0.1248 + 21.00 1.565 0.3447 -0.1317 + 22.00 1.563 0.3820 -0.1385 + 23.00 1.558 0.4203 -0.1452 + 24.00 1.552 0.4593 -0.1518 + 25.00 1.546 0.4988 -0.1583 + 26.00 1.539 0.5387 -0.1647 + 28.00 1.527 0.6187 -0.1770 + 30.00 1.522 0.6978 -0.1886 + 32.00 1.529 0.7747 -0.1994 + 35.00 1.544 0.8869 -0.2148 + 40.00 1.529 1.0671 -0.2392 + 45.00 1.471 1.2319 -0.2622 + 50.00 1.376 1.3747 -0.2839 + 55.00 1.249 1.4899 -0.3043 + 60.00 1.097 1.5728 -0.3236 + 65.00 0.928 1.6202 -0.3417 + 70.00 0.750 1.6302 -0.3586 + 75.00 0.570 1.6031 -0.3745 + 80.00 0.396 1.5423 -0.3892 + 85.00 0.237 1.4598 -0.4028 + 90.00 0.101 1.4041 -0.4151 + 95.00 -0.022 1.4053 -0.4261 + 100.00 -0.143 1.3914 -0.4357 + 105.00 -0.261 1.3625 -0.4437 + 110.00 -0.374 1.3188 -0.4498 + 115.00 -0.480 1.2608 -0.4538 + 120.00 -0.575 1.1891 -0.4553 + 125.00 -0.659 1.1046 -0.4540 + 130.00 -0.727 1.0086 -0.4492 + 135.00 -0.778 0.9025 -0.4405 + 140.00 -0.809 0.7883 -0.4270 + 145.00 -0.818 0.6684 -0.4078 + 150.00 -0.800 0.5457 -0.3821 + 155.00 -0.754 0.4236 -0.3484 + 160.00 -0.677 0.3066 -0.3054 + 170.00 -0.417 0.1085 -0.1842 + 175.00 -0.229 0.0510 -0.1013 + 180.00 0.000 0.0407 0.0000 diff --git a/examples/FAST.Farm_interface/inputs/FFFiles/Airfoils/DU35_A17_coords.txt b/examples/FAST.Farm_interface/inputs/FFFiles/Airfoils/DU35_A17_coords.txt new file mode 100644 index 00000000..5d3f84e8 --- /dev/null +++ b/examples/FAST.Farm_interface/inputs/FFFiles/Airfoils/DU35_A17_coords.txt @@ -0,0 +1,407 @@ + 400 NumCoords ! The number of coordinates in the airfoil shape file (including an extra coordinate for airfoil reference). Set to zero if coordinates not included. +! ......... x-y coordinates are next if NumCoords > 0 ............. +! x-y coordinate of airfoil reference +! x/c y/c +0.25 0 +! coordinates of airfoil shape; data from TU Delft as posted here: https://wind.nrel.gov/forum/wind/viewtopic.php?f=2&t=440 +! Adjusted DU 35 +! x/c y/c +1.00000 0.00283 +0.99660 0.00378 +0.99314 0.00477 +0.98961 0.00578 +0.98601 0.00683 +0.98235 0.00789 +0.97863 0.00897 +0.97484 0.01006 +0.97098 0.01116 +0.96706 0.01228 +0.96307 0.01342 +0.95902 0.01456 +0.95490 0.01571 +0.95072 0.01688 +0.94647 0.01806 +0.94216 0.01926 +0.93778 0.02046 +0.93333 0.02169 +0.92882 0.02292 +0.92425 0.02419 +0.91961 0.02547 +0.91490 0.02675 +0.91013 0.02807 +0.90529 0.02941 +0.90039 0.03077 +0.89542 0.03214 +0.89039 0.03353 +0.88529 0.03495 +0.88013 0.03638 +0.87490 0.03782 +0.86961 0.03929 +0.86425 0.04079 +0.85882 0.04230 +0.85333 0.04383 +0.84778 0.04538 +0.84216 0.04694 +0.83647 0.04853 +0.83072 0.05013 +0.82490 0.05176 +0.81902 0.05340 +0.81307 0.05506 +0.80706 0.05673 +0.80098 0.05842 +0.79484 0.06013 +0.78863 0.06184 +0.78235 0.06358 +0.77601 0.06531 +0.76961 0.06708 +0.76314 0.06885 +0.75660 0.07064 +0.75000 0.07244 +0.74333 0.07426 +0.73667 0.07606 +0.73000 0.07786 +0.72333 0.07966 +0.71667 0.08144 +0.71000 0.08322 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-0.00283 diff --git a/examples/FAST.Farm_interface/inputs/FFFiles/Airfoils/DU40_A17.dat b/examples/FAST.Farm_interface/inputs/FFFiles/Airfoils/DU40_A17.dat new file mode 100644 index 00000000..54a6d4ac --- /dev/null +++ b/examples/FAST.Farm_interface/inputs/FFFiles/Airfoils/DU40_A17.dat @@ -0,0 +1,190 @@ +! ------------ AirfoilInfo v1.01.x Input File ---------------------------------- +! DU40 airfoil with an aspect ratio of 17. Original -180 to 180deg Cl, Cd, and Cm versus AOA data taken from Appendix A of DOWEC document 10046_009.pdf (numerical values obtained from Koert Lindenburg of ECN). +! Cl and Cd values corrected for rotational stall delay and Cd values corrected using the Viterna method for 0 to 90deg AOA by Jason Jonkman using AirfoilPrep_v2p0.xls. +! note that this file uses Marshall Buhl's new input file processing; start all comment lines with ! +! ------------------------------------------------------------------------------ +"DEFAULT" InterpOrd ! Interpolation order to use for quasi-steady table lookup {1=linear; 3=cubic spline; "default"} [default=1] + 1 NonDimArea ! The non-dimensional area of the airfoil (area/chord^2) (set to 1.0 if unsure or unneeded) +@"DU40_A17_coords.txt" NumCoords ! The number of coordinates in the airfoil shape file. Set to zero if coordinates not included. +"unused" BL_file ! The file name including the boundary layer characteristics of the profile. Ignored if the aeroacoustic module is not called. + 1 NumTabs ! Number of airfoil tables in this file. +! ------------------------------------------------------------------------------ +! data for table 1 +! ------------------------------------------------------------------------------ + 0.75 Re ! Reynolds number in millions + 0 UserProp ! User property (control) setting +True InclUAdata ! Is unsteady aerodynamics data included in this table? If TRUE, then include 30 UA coefficients below this line +!........................................ + -3.2 alpha0 ! 0-lift angle of attack, depends on airfoil. + 9 alpha1 ! Angle of attack at f=0.7, (approximately the stall angle) for AOA>alpha0. (deg) + -9 alpha2 ! Angle of attack at f=0.7, (approximately the stall angle) for AOA1] + 0 S2 ! Constant in the f curve best-fit for AOA> alpha1; by definition it depends on the airfoil. [ignored if UAMod<>1] + 0 S3 ! Constant in the f curve best-fit for alpha2<=AOA< alpha0; by definition it depends on the airfoil. [ignored if UAMod<>1] + 0 S4 ! Constant in the f curve best-fit for AOA< alpha2; by definition it depends on the airfoil. [ignored if UAMod<>1] + 1.3519 Cn1 ! Critical value of C0n at leading edge separation. It should be extracted from airfoil data at a given Mach and Reynolds number. It can be calculated from the static value of Cn at either the break in the pitching moment or the loss of chord force at the onset of stall. It is close to the condition of maximum lift of the airfoil at low Mach numbers. + -0.3226 Cn2 ! As Cn1 for negative AOAs. + 0.19 St_sh ! Strouhal's shedding frequency constant. [default = 0.19] + 0.03 Cd0 ! 2D drag coefficient value at 0-lift. + -0.05 Cm0 ! 2D pitching moment coefficient about 1/4-chord location, at 0-lift, positive if nose up. [If the aerodynamics coefficients table does not include a column for Cm, this needs to be set to 0.0] + 0 k0 ! Constant in the \hat(x)_cp curve best-fit; = (\hat(x)_AC-0.25). [ignored if UAMod<>1] + 0 k1 ! Constant in the \hat(x)_cp curve best-fit. [ignored if UAMod<>1] + 0 k2 ! Constant in the \hat(x)_cp curve best-fit. [ignored if UAMod<>1] + 0 k3 ! Constant in the \hat(x)_cp curve best-fit. [ignored if UAMod<>1] + 0 k1_hat ! Constant in the expression of Cc due to leading edge vortex effects. [ignored if UAMod<>1] + 0.2 x_cp_bar ! Constant in the expression of \hat(x)_cp^v. [ignored if UAMod<>1, default = 0.2] +"DEFAULT" UACutout ! Angle of attack above which unsteady aerodynamics are disabled (deg). [Specifying the string "Default" sets UACutout to 45 degrees] +"DEFAULT" filtCutOff ! Reduced frequency cut-off for low-pass filtering the AoA input to UA, as well as the 1st and 2nd derivatives (-) [default = 0.5] +!........................................ +! Table of aerodynamics coefficients + 136 NumAlf ! Number of data lines in the following table +! Alpha Cl Cd Cm +! (deg) (-) (-) (-) + -180.00 0.000 0.0602 0.0000 + -175.00 0.218 0.0699 0.0934 + -170.00 0.397 0.1107 0.1697 + -160.00 0.642 0.3045 0.2813 + -155.00 0.715 0.4179 0.3208 + -150.00 0.757 0.5355 0.3516 + -145.00 0.772 0.6535 0.3752 + -140.00 0.762 0.7685 0.3926 + -135.00 0.731 0.8777 0.4048 + -130.00 0.680 0.9788 0.4126 + -125.00 0.613 1.0700 0.4166 + -120.00 0.532 1.1499 0.4176 + -115.00 0.439 1.2174 0.4158 + -110.00 0.337 1.2716 0.4117 + -105.00 0.228 1.3118 0.4057 + -100.00 0.114 1.3378 0.3979 + -95.00 -0.002 1.3492 0.3887 + -90.00 -0.120 1.3460 0.3781 + -85.00 -0.236 1.3283 0.3663 + -80.00 -0.349 1.2964 0.3534 + -75.00 -0.456 1.2507 0.3394 + -70.00 -0.557 1.1918 0.3244 + -65.00 -0.647 1.1204 0.3084 + -60.00 -0.727 1.0376 0.2914 + -55.00 -0.792 0.9446 0.2733 + -50.00 -0.842 0.8429 0.2543 + -45.00 -0.874 0.7345 0.2342 + -40.00 -0.886 0.6215 0.2129 + -35.00 -0.875 0.5067 0.1906 + -30.00 -0.839 0.3932 0.1670 + -25.00 -0.777 0.2849 0.1422 + -24.00 -0.761 0.2642 0.1371 + -23.00 -0.744 0.2440 0.1320 + -22.00 -0.725 0.2242 0.1268 + -21.00 -0.706 0.2049 0.1215 + -20.00 -0.685 0.1861 0.1162 + -19.00 -0.662 0.1687 0.1097 + -18.00 -0.635 0.1533 0.1012 + -17.00 -0.605 0.1398 0.0907 + -16.00 -0.571 0.1281 0.0784 + -15.00 -0.534 0.1183 0.0646 + -14.00 -0.494 0.1101 0.0494 + -13.00 -0.452 0.1036 0.0330 + -12.00 -0.407 0.0986 0.0156 + -11.00 -0.360 0.0951 -0.0026 + -10.00 -0.311 0.0931 -0.0213 + -8.00 -0.208 0.0930 -0.0600 + -6.00 -0.111 0.0689 -0.0500 + -5.50 -0.090 0.0614 -0.0516 + -5.00 -0.072 0.0547 -0.0532 + -4.50 -0.065 0.0480 -0.0538 + -4.00 -0.054 0.0411 -0.0544 + -3.50 -0.017 0.0349 -0.0554 + -3.00 0.003 0.0299 -0.0558 + -2.50 0.014 0.0255 -0.0555 + -2.00 0.009 0.0198 -0.0534 + -1.50 0.004 0.0164 -0.0442 + -1.00 0.036 0.0147 -0.0469 + -0.50 0.073 0.0137 -0.0522 + 0.00 0.137 0.0113 -0.0573 + 0.50 0.213 0.0114 -0.0644 + 1.00 0.292 0.0118 -0.0718 + 1.50 0.369 0.0122 -0.0783 + 2.00 0.444 0.0124 -0.0835 + 2.50 0.514 0.0124 -0.0866 + 3.00 0.580 0.0123 -0.0887 + 3.50 0.645 0.0120 -0.0900 + 4.00 0.710 0.0119 -0.0914 + 4.50 0.776 0.0122 -0.0933 + 5.00 0.841 0.0125 -0.0947 + 5.50 0.904 0.0129 -0.0957 + 6.00 0.967 0.0135 -0.0967 + 6.50 1.027 0.0144 -0.0973 + 7.00 1.084 0.0158 -0.0972 + 7.50 1.140 0.0174 -0.0972 + 8.00 1.193 0.0198 -0.0968 + 8.50 1.242 0.0231 -0.0958 + 9.00 1.287 0.0275 -0.0948 + 9.50 1.333 0.0323 -0.0942 + 10.00 1.368 0.0393 -0.0926 + 10.50 1.400 0.0475 -0.0908 + 11.00 1.425 0.0580 -0.0890 + 11.50 1.449 0.0691 -0.0877 + 12.00 1.473 0.0816 -0.0870 + 12.50 1.494 0.0973 -0.0870 + 13.00 1.513 0.1129 -0.0876 + 13.50 1.538 0.1288 -0.0886 + 14.50 1.587 0.1650 -0.0917 + 15.00 1.614 0.1845 -0.0939 + 15.50 1.631 0.2052 -0.0966 + 16.00 1.649 0.2250 -0.0996 + 16.50 1.666 0.2467 -0.1031 + 17.00 1.681 0.2684 -0.1069 + 17.50 1.699 0.2900 -0.1110 + 18.00 1.719 0.3121 -0.1157 + 19.00 1.751 0.3554 -0.1242 + 19.50 1.767 0.3783 -0.1291 + 20.50 1.798 0.4212 -0.1384 + 21.00 1.810 0.4415 -0.1416 + 22.00 1.830 0.4830 -0.1479 + 23.00 1.847 0.5257 -0.1542 + 24.00 1.861 0.5694 -0.1603 + 25.00 1.872 0.6141 -0.1664 + 26.00 1.881 0.6593 -0.1724 + 28.00 1.894 0.7513 -0.1841 + 30.00 1.904 0.8441 -0.1954 + 32.00 1.915 0.9364 -0.2063 + 35.00 1.929 1.0722 -0.2220 + 40.00 1.903 1.2873 -0.2468 + 45.00 1.820 1.4796 -0.2701 + 50.00 1.690 1.6401 -0.2921 + 55.00 1.522 1.7609 -0.3127 + 60.00 1.323 1.8360 -0.3321 + 65.00 1.106 1.8614 -0.3502 + 70.00 0.880 1.8347 -0.3672 + 75.00 0.658 1.7567 -0.3830 + 80.00 0.449 1.6334 -0.3977 + 85.00 0.267 1.4847 -0.4112 + 90.00 0.124 1.3879 -0.4234 + 95.00 0.002 1.3912 -0.4343 + 100.00 -0.118 1.3795 -0.4437 + 105.00 -0.235 1.3528 -0.4514 + 110.00 -0.348 1.3114 -0.4573 + 115.00 -0.453 1.2557 -0.4610 + 120.00 -0.549 1.1864 -0.4623 + 125.00 -0.633 1.1041 -0.4606 + 130.00 -0.702 1.0102 -0.4554 + 135.00 -0.754 0.9060 -0.4462 + 140.00 -0.787 0.7935 -0.4323 + 145.00 -0.797 0.6750 -0.4127 + 150.00 -0.782 0.5532 -0.3863 + 155.00 -0.739 0.4318 -0.3521 + 160.00 -0.664 0.3147 -0.3085 + 170.00 -0.410 0.1144 -0.1858 + 175.00 -0.226 0.0702 -0.1022 + 180.00 0.000 0.0602 0.0000 diff --git a/examples/FAST.Farm_interface/inputs/FFFiles/Airfoils/DU40_A17_coords.txt b/examples/FAST.Farm_interface/inputs/FFFiles/Airfoils/DU40_A17_coords.txt new file mode 100644 index 00000000..18d11b7b --- /dev/null +++ b/examples/FAST.Farm_interface/inputs/FFFiles/Airfoils/DU40_A17_coords.txt @@ -0,0 +1,407 @@ + 400 NumCoords ! The number of coordinates in the airfoil shape file (including an extra coordinate for airfoil reference). Set to zero if coordinates not included. +! ......... x-y coordinates are next if NumCoords > 0 ............. +! x-y coordinate of airfoil reference +! x/c y/c +0.33087 0 +! coordinates of airfoil shape; data from TU Delft as posted here: https://wind.nrel.gov/forum/wind/viewtopic.php?f=2&t=440 +! 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-0.00347 diff --git a/examples/FAST.Farm_interface/inputs/FFFiles/Airfoils/NACA64_A17.dat b/examples/FAST.Farm_interface/inputs/FFFiles/Airfoils/NACA64_A17.dat new file mode 100644 index 00000000..b9dca301 --- /dev/null +++ b/examples/FAST.Farm_interface/inputs/FFFiles/Airfoils/NACA64_A17.dat @@ -0,0 +1,181 @@ +! ------------ AirfoilInfo v1.01.x Input File ---------------------------------- +! NACA64 airfoil with an aspect ratio of 17. Original -180 to 180deg Cl, Cd, and Cm versus AOA data taken from Appendix A of DOWEC document 10046_009.pdf (numerical values obtained from Koert Lindenburg of ECN). +! Cl and Cd values corrected for rotational stall delay and Cd values corrected using the Viterna method for 0 to 90deg AOA by Jason Jonkman using AirfoilPrep_v2p0.xls. +! note that this file uses Marshall Buhl's new input file processing; start all comment lines with ! +! ------------------------------------------------------------------------------ +"DEFAULT" InterpOrd ! Interpolation order to use for quasi-steady table lookup {1=linear; 3=cubic spline; "default"} [default=1] + 1 NonDimArea ! The non-dimensional area of the airfoil (area/chord^2) (set to 1.0 if unsure or unneeded) +@"NACA64_A17_coords.txt" NumCoords ! The number of coordinates in the airfoil shape file. Set to zero if coordinates not included. +"unused" BL_file ! The file name including the boundary layer characteristics of the profile. Ignored if the aeroacoustic module is not called. + 1 NumTabs ! Number of airfoil tables in this file. +! ------------------------------------------------------------------------------ +! data for table 1 +! ------------------------------------------------------------------------------ + 0.75 Re ! Reynolds number in millions + 0 UserProp ! User property (control) setting +True InclUAdata ! Is unsteady aerodynamics data included in this table? If TRUE, then include 30 UA coefficients below this line +!........................................ + -4.432 alpha0 ! 0-lift angle of attack, depends on airfoil. + 9 alpha1 ! Angle of attack at f=0.7, (approximately the stall angle) for AOA>alpha0. (deg) + -9 alpha2 ! Angle of attack at f=0.7, (approximately the stall angle) for AOA1] + 0 S2 ! Constant in the f curve best-fit for AOA> alpha1; by definition it depends on the airfoil. [ignored if UAMod<>1] + 0 S3 ! Constant in the f curve best-fit for alpha2<=AOA< alpha0; by definition it depends on the airfoil. [ignored if UAMod<>1] + 0 S4 ! Constant in the f curve best-fit for AOA< alpha2; by definition it depends on the airfoil. [ignored if UAMod<>1] + 1.4073 Cn1 ! Critical value of C0n at leading edge separation. It should be extracted from airfoil data at a given Mach and Reynolds number. It can be calculated from the static value of Cn at either the break in the pitching moment or the loss of chord force at the onset of stall. It is close to the condition of maximum lift of the airfoil at low Mach numbers. + -0.7945 Cn2 ! As Cn1 for negative AOAs. + 0.19 St_sh ! Strouhal's shedding frequency constant. [default = 0.19] + 0.0065 Cd0 ! 2D drag coefficient value at 0-lift. + -0.088 Cm0 ! 2D pitching moment coefficient about 1/4-chord location, at 0-lift, positive if nose up. [If the aerodynamics coefficients table does not include a column for Cm, this needs to be set to 0.0] + 0 k0 ! Constant in the \hat(x)_cp curve best-fit; = (\hat(x)_AC-0.25). [ignored if UAMod<>1] + 0 k1 ! Constant in the \hat(x)_cp curve best-fit. [ignored if UAMod<>1] + 0 k2 ! Constant in the \hat(x)_cp curve best-fit. [ignored if UAMod<>1] + 0 k3 ! Constant in the \hat(x)_cp curve best-fit. [ignored if UAMod<>1] + 0 k1_hat ! Constant in the expression of Cc due to leading edge vortex effects. [ignored if UAMod<>1] +"Default" x_cp_bar ! Constant in the expression of \hat(x)_cp^v. [ignored if UAMod<>1, default = 0.2] +"Default" UACutout ! Angle of attack above which unsteady aerodynamics are disabled (deg). [Specifying the string "Default" sets UACutout to 45 degrees] +"DEFAULT" filtCutOff ! Reduced frequency cut-off for low-pass filtering the AoA input to UA, as well as the 1st and 2nd derivatives (-) [default = 0.5] +!........................................ +! Table of aerodynamics coefficients + 127 NumAlf ! Number of data lines in the following table +! Alpha Cl Cd Cm +! (deg) (-) (-) (-) + -180.00 0.000 0.0198 0.0000 + -175.00 0.374 0.0341 0.1880 + -170.00 0.749 0.0955 0.3770 + -160.00 0.659 0.2807 0.2747 + -155.00 0.736 0.3919 0.3130 + -150.00 0.783 0.5086 0.3428 + -145.00 0.803 0.6267 0.3654 + -140.00 0.798 0.7427 0.3820 + -135.00 0.771 0.8537 0.3935 + -130.00 0.724 0.9574 0.4007 + -125.00 0.660 1.0519 0.4042 + -120.00 0.581 1.1355 0.4047 + -115.00 0.491 1.2070 0.4025 + -110.00 0.390 1.2656 0.3981 + -105.00 0.282 1.3104 0.3918 + -100.00 0.169 1.3410 0.3838 + -95.00 0.052 1.3572 0.3743 + -90.00 -0.067 1.3587 0.3636 + -85.00 -0.184 1.3456 0.3517 + -80.00 -0.299 1.3181 0.3388 + -75.00 -0.409 1.2765 0.3248 + -70.00 -0.512 1.2212 0.3099 + -65.00 -0.606 1.1532 0.2940 + -60.00 -0.689 1.0731 0.2772 + -55.00 -0.759 0.9822 0.2595 + -50.00 -0.814 0.8820 0.2409 + -45.00 -0.850 0.7742 0.2212 + -40.00 -0.866 0.6610 0.2006 + -35.00 -0.860 0.5451 0.1789 + -30.00 -0.829 0.4295 0.1563 + -25.00 -0.853 0.3071 0.1156 + -24.00 -0.870 0.2814 0.1040 + -23.00 -0.890 0.2556 0.0916 + -22.00 -0.911 0.2297 0.0785 + -21.00 -0.934 0.2040 0.0649 + -20.00 -0.958 0.1785 0.0508 + -19.00 -0.982 0.1534 0.0364 + -18.00 -1.005 0.1288 0.0218 + -17.00 -1.082 0.1037 0.0129 + -16.00 -1.113 0.0786 -0.0028 + -15.00 -1.105 0.0535 -0.0251 + -14.00 -1.078 0.0283 -0.0419 + -13.50 -1.053 0.0158 -0.0521 + -13.00 -1.015 0.0151 -0.0610 + -12.00 -0.904 0.0134 -0.0707 + -11.00 -0.807 0.0121 -0.0722 + -10.00 -0.711 0.0111 -0.0734 + -9.00 -0.595 0.0099 -0.0772 + -8.00 -0.478 0.0091 -0.0807 + -7.00 -0.375 0.0086 -0.0825 + -6.00 -0.264 0.0082 -0.0832 + -5.00 -0.151 0.0079 -0.0841 + -4.00 -0.017 0.0072 -0.0869 + -3.00 0.088 0.0064 -0.0912 + -2.00 0.213 0.0054 -0.0946 + -1.00 0.328 0.0052 -0.0971 + 0.00 0.442 0.0052 -0.1014 + 1.00 0.556 0.0052 -0.1076 + 2.00 0.670 0.0053 -0.1126 + 3.00 0.784 0.0053 -0.1157 + 4.00 0.898 0.0054 -0.1199 + 5.00 1.011 0.0058 -0.1240 + 6.00 1.103 0.0091 -0.1234 + 7.00 1.181 0.0113 -0.1184 + 8.00 1.257 0.0124 -0.1163 + 8.50 1.293 0.0130 -0.1163 + 9.00 1.326 0.0136 -0.1160 + 9.50 1.356 0.0143 -0.1154 + 10.00 1.382 0.0150 -0.1149 + 10.50 1.400 0.0267 -0.1145 + 11.00 1.415 0.0383 -0.1143 + 11.50 1.425 0.0498 -0.1147 + 12.00 1.434 0.0613 -0.1158 + 12.50 1.443 0.0727 -0.1165 + 13.00 1.451 0.0841 -0.1153 + 13.50 1.453 0.0954 -0.1131 + 14.00 1.448 0.1065 -0.1112 + 14.50 1.444 0.1176 -0.1101 + 15.00 1.445 0.1287 -0.1103 + 15.50 1.447 0.1398 -0.1109 + 16.00 1.448 0.1509 -0.1114 + 16.50 1.444 0.1619 -0.1111 + 17.00 1.438 0.1728 -0.1097 + 17.50 1.439 0.1837 -0.1079 + 18.00 1.448 0.1947 -0.1080 + 18.50 1.452 0.2057 -0.1090 + 19.00 1.448 0.2165 -0.1086 + 19.50 1.438 0.2272 -0.1077 + 20.00 1.428 0.2379 -0.1099 + 21.00 1.401 0.2590 -0.1169 + 22.00 1.359 0.2799 -0.1190 + 23.00 1.300 0.3004 -0.1235 + 24.00 1.220 0.3204 -0.1393 + 25.00 1.168 0.3377 -0.1440 + 26.00 1.116 0.3554 -0.1486 + 28.00 1.015 0.3916 -0.1577 + 30.00 0.926 0.4294 -0.1668 + 32.00 0.855 0.4690 -0.1759 + 35.00 0.800 0.5324 -0.1897 + 40.00 0.804 0.6452 -0.2126 + 45.00 0.793 0.7573 -0.2344 + 50.00 0.763 0.8664 -0.2553 + 55.00 0.717 0.9708 -0.2751 + 60.00 0.656 1.0693 -0.2939 + 65.00 0.582 1.1606 -0.3117 + 70.00 0.495 1.2438 -0.3285 + 75.00 0.398 1.3178 -0.3444 + 80.00 0.291 1.3809 -0.3593 + 85.00 0.176 1.4304 -0.3731 + 90.00 0.053 1.4565 -0.3858 + 95.00 -0.074 1.4533 -0.3973 + 100.00 -0.199 1.4345 -0.4075 + 105.00 -0.321 1.4004 -0.4162 + 110.00 -0.436 1.3512 -0.4231 + 115.00 -0.543 1.2874 -0.4280 + 120.00 -0.640 1.2099 -0.4306 + 125.00 -0.723 1.1196 -0.4304 + 130.00 -0.790 1.0179 -0.4270 + 135.00 -0.840 0.9064 -0.4196 + 140.00 -0.868 0.7871 -0.4077 + 145.00 -0.872 0.6627 -0.3903 + 150.00 -0.850 0.5363 -0.3665 + 155.00 -0.798 0.4116 -0.3349 + 160.00 -0.714 0.2931 -0.2942 + 170.00 -0.749 0.0971 -0.3771 + 175.00 -0.374 0.0334 -0.1879 + 180.00 0.000 0.0198 0.0000 diff --git a/examples/FAST.Farm_interface/inputs/FFFiles/Airfoils/NACA64_A17_coords.txt b/examples/FAST.Farm_interface/inputs/FFFiles/Airfoils/NACA64_A17_coords.txt new file mode 100644 index 00000000..b2b49e07 --- /dev/null +++ b/examples/FAST.Farm_interface/inputs/FFFiles/Airfoils/NACA64_A17_coords.txt @@ -0,0 +1,407 @@ + 400 NumCoords ! The number of coordinates in the airfoil shape file (including an extra coordinate for airfoil reference). Set to zero if coordinates not included. +! ......... x-y coordinates are next if NumCoords > 0 ............. +! x-y coordinate of airfoil reference +! x/c y/c +0.25 0 +! coordinates of airfoil shape; data from TU Delft as posted here: https://wind.nrel.gov/forum/wind/viewtopic.php?f=2&t=440 +! NACA 64-618 (interpolated to 399 points) +! x/c y/c +1.000000 0.000000 +0.990000 0.003385 +0.980000 0.006126 +0.975000 0.007447 +0.970000 0.008767 +0.965000 0.010062 +0.960000 0.011357 +0.955000 0.012639 +0.950000 0.013921 +0.945000 0.015200 +0.940000 0.016478 +0.935000 0.017757 +0.930000 0.019036 +0.925000 0.020317 +0.920000 0.021598 +0.915000 0.022881 +0.910000 0.024163 +0.905000 0.025448 +0.900000 0.026733 +0.887500 0.029951 +0.875000 0.033169 +0.862500 0.036386 +0.850000 0.039603 +0.837500 0.042804 +0.825000 0.046004 +0.812500 0.049171 +0.800000 0.052337 +0.787500 0.055452 +0.775000 0.058566 +0.762500 0.061611 +0.750000 0.064656 +0.737500 0.067615 +0.725000 0.070573 +0.712500 0.073429 +0.700000 0.076285 +0.687500 0.079029 +0.675000 0.081773 +0.662500 0.084393 +0.650000 0.087012 +0.637500 0.089490 +0.625000 0.091967 +0.612500 0.094283 +0.600000 0.096599 +0.587500 0.098743 +0.575000 0.100887 +0.562500 0.102843 +0.550000 0.104799 +0.537500 0.106549 +0.525000 0.108299 +0.512500 0.109830 +0.500000 0.111360 +0.487500 0.112649 +0.475000 0.113937 +0.462500 0.114964 +0.450000 0.115990 +0.445000 0.116320 +0.440000 0.116650 +0.435000 0.116931 +0.430000 0.117211 +0.425000 0.117439 +0.420000 0.117667 +0.415000 0.117835 +0.410000 0.118003 +0.405000 0.118104 +0.400000 0.118204 +0.395000 0.118231 +0.390000 0.118258 +0.385000 0.118213 +0.380000 0.118168 +0.375000 0.118057 +0.370000 0.117946 +0.365000 0.117777 +0.360000 0.117607 +0.355000 0.117383 +0.350000 0.117159 +0.345000 0.116881 +0.340000 0.116603 +0.335000 0.116273 +0.330000 0.115942 +0.325000 0.115562 +0.320000 0.115181 +0.315000 0.114750 +0.310000 0.114319 +0.305000 0.113838 +0.300000 0.113356 +0.295000 0.112824 +0.290000 0.112292 +0.285000 0.111710 +0.280000 0.111127 +0.275000 0.110495 +0.270000 0.109863 +0.265000 0.109180 +0.260000 0.108497 +0.255000 0.107762 +0.250000 0.107027 +0.245000 0.106241 +0.240000 0.105454 +0.235000 0.104614 +0.230000 0.103774 +0.225000 0.102880 +0.220000 0.101985 +0.215000 0.101035 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-0.036486 +0.612500 -0.034526 +0.625000 -0.032565 +0.637500 -0.030575 +0.650000 -0.028585 +0.662500 -0.026594 +0.675000 -0.024603 +0.687500 -0.022632 +0.700000 -0.020660 +0.712500 -0.018728 +0.725000 -0.016795 +0.737500 -0.014922 +0.750000 -0.013048 +0.762500 -0.011260 +0.775000 -0.009472 +0.787500 -0.007797 +0.800000 -0.006122 +0.812500 -0.004594 +0.825000 -0.003065 +0.837500 -0.001721 +0.850000 -0.000376 +0.862500 0.000742 +0.875000 0.001859 +0.887500 0.002698 +0.900000 0.003536 +0.905000 0.003780 +0.910000 0.004023 +0.915000 0.004205 +0.920000 0.004387 +0.925000 0.004504 +0.930000 0.004620 +0.935000 0.004661 +0.940000 0.004702 +0.945000 0.004658 +0.950000 0.004614 +0.955000 0.004476 +0.960000 0.004338 +0.965000 0.004084 +0.970000 0.003829 +0.975000 0.003436 +0.980000 0.003042 +0.990000 0.001910 +1.000000 0.000000 diff --git a/examples/FAST.Farm_interface/inputs/FFFiles/Cp_Ct_Cq.NREL5MW.txt b/examples/FAST.Farm_interface/inputs/FFFiles/Cp_Ct_Cq.NREL5MW.txt new file mode 100644 index 00000000..4324d3bb --- /dev/null +++ b/examples/FAST.Farm_interface/inputs/FFFiles/Cp_Ct_Cq.NREL5MW.txt @@ -0,0 +1,99 @@ +# ----- Rotor performance tables for the NREL-5MW wind turbine ----- +# ------------ Written on Jan-13-22 using the ROSCO toolbox ------------ + +# Pitch angle vector, 36 entries - x axis (matrix columns) (deg) +-5.0 -4.0 -3.0 -2.0 -1.0 0.0 1.0 2.0 3.0 4.0 5.0 6.0 7.0 8.0 9.0 10.0 11.0 12.0 13.0 14.0 15.0 16.0 17.0 18.0 19.0 20.0 21.0 22.0 23.0 24.0 25.0 26.0 27.0 28.0 29.0 30.0 +# TSR vector, 26 entries - y axis (matrix rows) (-) +2.0 2.5 3.0 3.5 4.0 4.5 5.0 5.5 6.0 6.5 7.0 7.5 8.0 8.5 9.0 9.5 10.0 10.5 11.0 11.5 12.0 12.5 13.0 13.5 14.0 14.5 +# Wind speed vector - z axis (m/s) +11.4 + +# Power coefficient + +0.006673 0.009813 0.013077 0.016508 0.020122 0.023918 0.027887 0.032006 0.036239 0.040540 0.044858 0.049138 0.053326 0.057366 0.061205 0.064796 0.068092 0.071051 0.073631 0.075796 0.077520 0.078793 0.079607 0.079960 0.079851 0.079303 0.078341 0.076993 0.075269 0.073154 0.070619 0.067607 0.064059 0.059976 0.055381 0.050328 +0.020093 0.026879 0.033876 0.041034 0.048264 0.055472 0.062560 0.069438 0.076024 0.082246 0.088041 0.093349 0.098111 0.102262 0.105746 0.108521 0.110563 0.111865 0.112435 0.112304 0.111503 0.110082 0.108043 0.105376 0.102031 0.097898 0.092907 0.087092 0.080496 0.073183 0.065206 0.056618 0.047499 0.037976 0.028144 0.018084 +0.048757 0.059921 0.070879 0.081507 0.091686 0.101314 0.110305 0.118583 0.126073 0.132692 0.138350 0.142964 0.146489 0.148944 0.150362 0.150761 0.150158 0.148560 0.145993 0.142397 0.137607 0.131540 0.124241 0.115747 0.106162 0.095542 0.084011 0.071754 0.058916 0.045611 0.031929 0.017939 0.003701 -0.010721 -0.025259 -0.039848 +0.090123 0.104877 0.118836 0.131894 0.143960 0.154953 0.164780 0.173312 0.180438 0.186134 0.190421 0.193294 0.194678 0.194534 0.192872 0.189595 0.184490 0.177562 0.168848 0.158486 0.146540 0.133154 0.118581 0.103012 0.086606 0.069499 0.051807 0.033628 0.015033 -0.003935 -0.023212 -0.042681 -0.062203 -0.081676 -0.101014 -0.120137 +0.139124 0.156683 0.172901 0.187702 0.200999 0.212709 0.222753 0.231064 0.237530 0.241950 0.244105 0.243810 0.240834 0.235185 0.226970 0.216406 0.203596 0.188826 0.172423 0.154596 0.135473 0.115192 0.093900 0.071756 0.048901 0.025448 0.001458 -0.023067 -0.048079 -0.073394 -0.098747 -0.123894 -0.148637 -0.172971 -0.196999 -0.220426 +0.191782 0.211839 0.230276 0.247076 0.262109 0.275108 0.285675 0.293225 0.297120 0.296898 0.292698 0.284905 0.273940 0.260137 0.243968 0.225765 0.205747 0.184044 0.160751 0.135955 0.109826 0.082563 0.054349 0.025323 -0.004446 -0.034984 -0.066317 -0.098275 -0.130442 -0.162296 -0.193412 -0.223707 -0.253665 -0.283545 -0.312671 -0.340141 +0.246353 0.270341 0.292682 0.312827 0.329812 0.342452 0.349588 0.350796 0.346468 0.337517 0.324917 0.309376 0.291272 0.270832 0.248190 0.223439 0.196656 0.167952 0.137415 0.105259 0.071726 0.037018 0.001262 -0.035533 -0.073456 -0.112507 -0.152329 -0.192145 -0.231094 -0.268667 -0.305110 -0.341553 -0.378474 -0.414899 -0.449086 -0.478908 +0.306243 0.335683 0.361286 0.381426 0.394666 0.400011 0.397807 0.389766 0.377676 0.362345 0.344063 0.323009 0.299287 0.272921 0.243930 0.212388 0.178407 0.142107 0.103741 0.063607 0.021945 -0.021117 -0.065611 -0.111678 -0.159287 -0.207873 -0.256248 -0.303158 -0.347971 -0.391262 -0.434965 -0.480253 -0.525739 -0.568955 -0.606708 -0.638532 +0.368062 0.397982 0.420678 0.434161 0.438041 0.434596 0.426094 0.413722 0.397833 0.378568 0.356023 0.330207 0.301063 0.268542 0.232706 0.193700 0.151740 0.107083 0.060108 0.011125 -0.039710 -0.092454 -0.147289 -0.204180 -0.262421 -0.320480 -0.376558 -0.429701 -0.480649 -0.532192 -0.586717 -0.643176 -0.698195 -0.746783 -0.788014 -0.825218 +0.413915 0.437699 0.451902 0.458070 0.457967 0.452866 0.443478 0.429833 0.411921 0.389793 0.363427 0.332762 0.297737 0.258384 0.214897 0.167596 0.116800 0.062939 0.006435 -0.052490 -0.113873 -0.177938 -0.244676 -0.313397 -0.382360 -0.449143 -0.512100 -0.571792 -0.631581 -0.695509 -0.764242 -0.833635 -0.896797 -0.950560 -0.998368 -1.044827 +0.427324 0.444280 0.455448 0.462056 0.464498 0.462253 0.454597 0.441298 0.422256 0.397517 0.367139 0.331124 0.289519 0.242518 0.190536 0.134077 0.073568 0.009566 -0.057573 -0.127803 -0.201376 -0.278345 -0.358171 -0.439117 -0.518328 -0.593032 -0.663068 -0.731776 -0.804602 -0.885395 -0.971040 -1.052725 -1.123154 -1.184540 -1.242706 -1.302084 +0.413889 0.430080 0.443986 0.455667 0.463490 0.465861 0.461379 0.449315 0.429515 0.402103 0.367325 0.325347 0.276400 0.220931 0.159637 0.093102 0.021935 -0.053297 -0.132381 -0.215535 -0.302917 -0.394172 -0.487834 -0.580989 -0.669719 -0.752399 -0.831452 -0.912845 -1.003839 -1.105589 -1.208911 -1.301214 -1.380509 -1.453087 -1.525242 -1.600224 +0.390738 0.409602 0.427384 0.443933 0.457445 0.465005 0.464411 0.454181 0.433864 0.403639 0.364016 0.315425 0.258360 0.193623 0.122136 0.044567 -0.038313 -0.126023 -0.218606 -0.316340 -0.419059 -0.525699 -0.633667 -0.738622 -0.836834 -0.928785 -1.019688 -1.118620 -1.233318 -1.358741 -1.478110 -1.581346 -1.672639 -1.759983 -1.849169 -1.941926 +0.363054 0.386720 0.409228 0.429996 0.447852 0.460425 0.463989 0.456010 0.435373 0.402165 0.357222 0.301344 0.235402 0.160566 0.077923 -0.011703 -0.107479 -0.209107 -0.316861 -0.430808 -0.550233 -0.673151 -0.795604 -0.912315 -1.020857 -1.123956 -1.230487 -1.353172 -1.496497 -1.645302 -1.779751 -1.896314 -2.002958 -2.108318 -2.217267 -2.330606 +0.332023 0.361556 0.389367 0.414649 0.436246 0.452807 0.460431 0.454894 0.434075 0.397696 0.346937 0.283092 0.207494 0.121668 0.026850 -0.075950 -0.185943 -0.303110 -0.427726 -0.559435 -0.696810 -0.836734 -0.973950 -1.103096 -1.222996 -1.339770 -1.467400 -1.620400 -1.794614 -1.965735 -2.116279 -2.249130 -2.374431 -2.500966 -2.632648 -2.770283 +0.297995 0.333854 0.367528 0.397656 0.423215 0.442899 0.454053 0.450936 0.429986 0.390235 0.333142 0.260640 0.174562 0.076794 -0.031277 -0.148468 -0.274167 -0.408575 -0.551737 -0.702675 -0.859149 -1.016871 -1.169580 -1.311915 -1.444423 -1.578792 -1.734397 -1.922541 -2.128205 -2.321411 -2.490350 -2.642587 -2.789846 -2.940844 -3.098986 -3.264660 +0.261597 0.303619 0.343502 0.378889 0.408674 0.431280 0.445167 0.444233 0.423112 0.379761 0.315806 0.233927 0.136491 0.025768 -0.096686 -0.229613 -0.372646 -0.526034 -0.689370 -0.860978 -1.037730 -1.214335 -1.383513 -1.539437 -1.686737 -1.844401 -2.034203 -2.260837 -2.498120 -2.714447 -2.904511 -3.079332 -3.251981 -3.431224 -3.619857 -3.816817 +0.223751 0.271311 0.317227 0.358217 0.392491 0.418111 0.434088 0.434927 0.413446 0.366239 0.294883 0.202866 0.093151 -0.031589 -0.169648 -0.319787 -0.481868 -0.655988 -0.841105 -1.034831 -1.233270 -1.430180 -1.616348 -1.786462 -1.952417 -2.139500 -2.368690 -2.636225 -2.905702 -3.147086 -3.361213 -3.561934 -3.763787 -3.975522 -4.198409 -4.429489 +0.185578 0.237532 0.288993 0.335546 0.374551 0.403289 0.421002 0.423063 0.400961 0.349628 0.270309 0.167352 0.044405 -0.095487 -0.250473 -0.419415 -0.602317 -0.798913 -1.007440 -1.224860 -1.446724 -1.665242 -1.868434 -2.054428 -2.244050 -2.466255 -2.739406 -3.049892 -3.352672 -3.621561 -3.862815 -4.093010 -4.328409 -4.576896 -4.837351 -5.105458 +0.147095 0.203239 0.259075 0.310894 0.354752 0.386719 0.405978 0.408744 0.385629 0.329881 0.242007 0.127271 -0.009910 -0.166158 -0.339498 -0.528928 -0.734472 -0.955298 -1.188911 -1.431845 -1.679152 -1.920015 -2.140330 -2.345296 -2.563821 -2.826409 -3.147779 -3.503220 -3.840906 -4.140058 -4.411660 -4.675361 -4.948974 -5.238172 -5.539321 -5.847566 +0.109921 0.168465 0.228283 0.284493 0.333003 0.368316 0.389001 0.392004 0.367452 0.306944 0.209888 0.082498 -0.069969 -0.243863 -0.437077 -0.648769 -0.878808 -1.125646 -1.386141 -1.656724 -1.931386 -2.194733 -2.433122 -2.661010 -2.913585 -3.221522 -3.595200 -3.997663 -4.372318 -4.704715 -5.010142 -5.311913 -5.628384 -5.961897 -6.307013 -6.658699 +0.075556 0.133907 0.196815 0.256499 0.309270 0.347981 0.370019 0.372880 0.346417 0.280755 0.173858 0.032901 -0.135979 -0.328881 -0.543585 -0.779386 -1.035790 -1.310469 -1.599847 -1.900506 -2.203972 -2.489774 -2.748220 -3.003362 -3.294941 -3.653136 -4.083147 -4.534716 -4.948847 -5.317645 -5.660775 -6.005570 -6.369299 -6.750614 -7.143160 -7.541782 +0.045437 0.101086 0.164731 0.227521 0.283675 0.325613 0.348964 0.351362 0.322521 0.251245 0.133815 -0.021672 -0.208162 -0.421508 -0.659413 -0.921225 -1.205892 -1.510319 -1.830843 -2.164074 -2.497172 -2.805822 -3.087060 -3.374013 -3.709339 -4.122787 -4.613131 -5.115993 -5.572447 -5.980987 -6.366170 -6.759084 -7.174174 -7.606904 -8.050518 -8.499762 +0.020095 0.070625 0.132961 0.197686 0.256313 0.301131 0.325760 0.327415 0.295744 0.218342 0.089649 -0.081378 -0.286748 -0.522056 -0.784958 -1.074719 -1.389587 -1.725804 -2.080005 -2.448103 -2.811255 -3.143907 -3.451088 -3.774480 -4.158169 -4.632027 -5.186626 -5.743189 -6.245055 -6.696930 -7.128978 -7.575043 -8.045426 -8.533374 -9.031865 -9.535604 +-0.001687 0.043909 0.102330 0.166837 0.227413 0.274487 0.300332 0.301010 0.266040 0.181968 0.041242 -0.146395 -0.371984 -0.630855 -0.920613 -1.240294 -1.587356 -1.957580 -2.348192 -2.753074 -3.146694 -3.505110 -3.841738 -4.206100 -4.642786 -5.182427 -5.805056 -6.418029 -6.968601 -7.467747 -7.951835 -8.455876 -8.985506 -9.532652 -10.089996 -10.652280 +-0.020991 0.020364 0.073330 0.135754 0.197326 0.245733 0.272607 0.272110 0.233378 0.142039 -0.011538 -0.216915 -0.464126 -0.748233 -1.066769 -1.418378 -1.799699 -2.206350 -2.636179 -3.079288 -3.504186 -3.890511 -4.260392 -4.670103 -5.164549 -5.775547 -6.469853 -7.142266 -7.745026 -8.295764 -8.837283 -9.403900 -9.996885 -10.607377 -11.227722 -11.852766 + + +# Thrust coefficient + +0.128717 0.128402 0.127976 0.127677 0.127561 0.127629 0.127867 0.128247 0.128729 0.129258 0.129777 0.130225 0.130542 0.130673 0.130570 0.130193 0.129510 0.128500 0.127155 0.125472 0.123467 0.121169 0.118605 0.115809 0.112801 0.109598 0.106205 0.102605 0.098769 0.094663 0.090253 0.085471 0.080247 0.074585 0.068519 0.062126 +0.168397 0.169715 0.171083 0.172538 0.173986 0.175323 0.176451 0.177284 0.177754 0.177804 0.177391 0.176487 0.175078 0.173164 0.170771 0.167935 0.164700 0.161125 0.157265 0.153157 0.148796 0.144149 0.139139 0.133696 0.127741 0.121140 0.113810 0.105805 0.097197 0.088074 0.078501 0.068532 0.058230 0.047709 0.037053 0.026331 +0.226643 0.229393 0.231723 0.233550 0.234756 0.235255 0.234993 0.233948 0.232126 0.229565 0.226326 0.222484 0.218143 0.213440 0.208473 0.203249 0.197693 0.191672 0.185067 0.177711 0.169360 0.159907 0.149434 0.138024 0.125825 0.112914 0.099398 0.085443 0.071172 0.056685 0.042068 0.027389 0.012700 -0.001958 -0.016522 -0.030881 +0.299075 0.301289 0.302422 0.302406 0.301210 0.298869 0.295464 0.291107 0.285985 0.280362 0.274473 0.268391 0.262007 0.255130 0.247532 0.238852 0.228637 0.216830 0.203516 0.188917 0.173159 0.156385 0.138854 0.120751 0.102214 0.083356 0.064271 0.045044 0.025754 0.006460 -0.012785 -0.031903 -0.050766 -0.069197 -0.086927 -0.103550 +0.379238 0.378835 0.376828 0.373306 0.368432 0.362520 0.355993 0.349221 0.342334 0.335182 0.327457 0.318711 0.308189 0.295450 0.280436 0.263431 0.244639 0.224405 0.203103 0.180973 0.158152 0.134784 0.110984 0.086862 0.062520 0.038061 0.013566 -0.010909 -0.035298 -0.059484 -0.083286 -0.106436 -0.128554 -0.149119 -0.167467 -0.182809 +0.462045 0.457610 0.451683 0.444801 0.437544 0.430278 0.422940 0.415089 0.406018 0.394702 0.380509 0.363246 0.343190 0.320701 0.296376 0.270674 0.243937 0.216365 0.188092 0.159188 0.129783 0.100004 0.069970 0.039795 0.009565 -0.020663 -0.050818 -0.080761 -0.110260 -0.138960 -0.166409 -0.192073 -0.215232 -0.234926 -0.250010 -0.259496 +0.545296 0.537969 0.530603 0.523523 0.516328 0.508094 0.497562 0.483752 0.466005 0.444344 0.419336 0.391808 0.362349 0.331374 0.299182 0.266026 0.232071 0.197454 0.162213 0.126478 0.090382 0.054055 0.017608 -0.018892 -0.055386 -0.091750 -0.127731 -0.162918 -0.196784 -0.228774 -0.258236 -0.284215 -0.305420 -0.320331 -0.327933 -0.328268 +0.634417 0.627969 0.621264 0.612780 0.601387 0.585824 0.565236 0.539859 0.510799 0.478901 0.444769 0.408839 0.371429 0.332767 0.293070 0.252557 0.211368 0.169524 0.127130 0.084335 0.041284 -0.001917 -0.045208 -0.088516 -0.131639 -0.174175 -0.215526 -0.255049 -0.292101 -0.325924 -0.355354 -0.378817 -0.394523 -0.401294 -0.399320 -0.390574 +0.735578 0.726839 0.715209 0.698962 0.676693 0.649128 0.617406 0.582286 0.544379 0.504195 0.462125 0.418443 0.373358 0.327062 0.279804 0.231775 0.183064 0.133686 0.083811 0.033605 -0.016820 -0.067406 -0.118066 -0.168514 -0.218193 -0.266339 -0.312201 -0.355042 -0.394026 -0.427876 -0.454896 -0.473018 -0.480617 -0.477721 -0.466483 -0.450923 +0.836616 0.819394 0.796306 0.768163 0.735696 0.699319 0.659490 0.616641 0.571164 0.523450 0.473790 0.422421 0.369559 0.315437 0.260360 0.204512 0.147873 0.090579 0.032826 -0.025256 -0.083602 -0.142121 -0.200467 -0.257947 -0.313640 -0.366661 -0.416171 -0.461284 -0.500752 -0.532889 -0.555398 -0.565981 -0.564006 -0.551394 -0.532762 -0.512992 +0.923379 0.893210 0.859907 0.823650 0.784285 0.741493 0.695217 0.645715 0.593258 0.538206 0.480917 0.421690 0.360798 0.298558 0.235326 0.171229 0.106253 0.040624 -0.025491 -0.092007 -0.158843 -0.225631 -0.291594 -0.355648 -0.416743 -0.473917 -0.526240 -0.572594 -0.611418 -0.640346 -0.656398 -0.657833 -0.645755 -0.624799 -0.601049 -0.579120 +0.993425 0.954344 0.913695 0.871240 0.826266 0.778188 0.726411 0.670805 0.611601 0.549205 0.484132 0.416794 0.347553 0.276858 0.205091 0.132281 0.058537 -0.015913 -0.090942 -0.166478 -0.242184 -0.317269 -0.390504 -0.460636 -0.526540 -0.587232 -0.641708 -0.688659 -0.725848 -0.749926 -0.757799 -0.749140 -0.727679 -0.700204 -0.673221 -0.650161 +1.058549 1.011415 0.963227 0.914208 0.863809 0.810735 0.753864 0.692505 0.626704 0.556910 0.483849 0.408103 0.330166 0.250636 0.169909 0.087938 0.004949 -0.078857 -0.163388 -0.248386 -0.333115 -0.416283 -0.496411 -0.572141 -0.642397 -0.706208 -0.762552 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-0.045104 -0.065821 -0.088677 -0.113491 -0.139960 -0.167888 -0.196836 -0.224978 -0.250604 -0.274671 -0.300722 -0.331943 -0.370526 -0.415042 -0.458867 -0.498231 -0.533919 -0.568529 -0.604567 -0.642433 -0.681552 -0.721401 -0.761602 +-0.001449 0.001406 0.005062 0.009371 0.013622 0.016963 0.018818 0.018784 0.016110 0.009805 -0.000797 -0.014974 -0.032039 -0.051651 -0.073640 -0.097912 -0.124235 -0.152307 -0.181979 -0.212567 -0.241898 -0.268567 -0.294100 -0.322383 -0.356515 -0.398693 -0.446622 -0.493039 -0.534649 -0.572667 -0.610048 -0.649163 -0.690097 -0.732240 -0.775063 -0.818211 + diff --git a/examples/FAST.Farm_interface/inputs/FFFiles/DISCON_WT1.IN b/examples/FAST.Farm_interface/inputs/FFFiles/DISCON_WT1.IN new file mode 100644 index 00000000..f686990d --- /dev/null +++ b/examples/FAST.Farm_interface/inputs/FFFiles/DISCON_WT1.IN @@ -0,0 +1,198 @@ +! Controller parameter input file for the FAST.Farm wind turbine +! - File written using ROSCO version 2.9.4 controller tuning logic on 10/11/25 + +!------- SIMULATION CONTROL ------------------------------------------------------------ +1 ! LoggingLevel - {0: write no debug files, 1: write standard output .dbg-file, 2: LoggingLevel 1 + ROSCO LocalVars (.dbg2) 3: LoggingLevel 2 + complete avrSWAP-array (.dbg3)} +0.0 ! DT_Out - {Time step to output .dbg* files, or 0 to match sampling period of OpenFAST} +1 ! Ext_Interface - (0 - use standard bladed interface, 1 - Use the extened DLL interface introduced in OpenFAST 3.5.0.) +0 ! Echo - (0 - no Echo, 1 - Echo input data to .echo) + +!------- CONTROLLER FLAGS ------------------------------------------------- +1 ! F_LPFType - (1: first-order low-pass filter, 2: second-order low-pass filter), [rad/s] (currently filters generator speed and pitch control signals +0 ! IPC_ControlMode - Turn Individual Pitch Control (IPC) for fatigue load reductions (pitch contribution) {0: off, 1: 1P reductions, 2: 1P+2P reductions} +3 ! VS_ControlMode - Generator torque control mode in above rated conditions (0- no torque control, 1- k*omega^2 with PI transitions, 2- WSE TSR Tracking, 3- Power-based TSR Tracking)} +0 ! VS_ConstPower - Do constant power torque control, where above rated torque varies, 0 for constant torque} +1 ! PC_ControlMode - Blade pitch control mode {0: No pitch, fix to fine pitch, 1: active PI blade pitch control} +0 ! Y_ControlMode - Yaw control mode {0: no yaw control, 1: yaw rate control, 2: yaw-by-IPC} +1 ! SS_Mode - Setpoint Smoother mode {0: no setpoint smoothing, 1: introduce setpoint smoothing} +0 ! PRC_Mode - Power reference tracking mode{0: use standard rotor speed set points, 1: use PRC rotor speed setpoints} +2 ! WE_Mode - Wind speed estimator mode {0: One-second low pass filtered hub height wind speed, 1: Immersion and Invariance Estimator, 2: Extended Kalman Filter} +1 ! PS_Mode - Pitch saturation mode {0: no pitch saturation, 1: implement pitch saturation} +0 ! SD_Mode - Shutdown mode {0: no shutdown procedure, 1: pitch to max pitch at shutdown} +0 ! Fl_Mode - Floating specific feedback mode {0: no nacelle velocity feedback, 1: feed back translational velocity, 2: feed back rotational veloicty} +0 ! TD_Mode - Tower damper mode (0- no tower damper, 1- feed back translational nacelle accelleration to pitch angle +0 ! TRA_Mode - Tower resonance avoidance mode (0- no tower resonsnace avoidance, 1- use torque control setpoints to avoid a specific frequency +0 ! Flp_Mode - Flap control mode {0: no flap control, 1: steady state flap angle, 2: Proportional flap control, 2: Cyclic (1P) flap control} +0 ! OL_Mode - Open loop control mode {0: no open loop control, 1: open loop control vs. time, 2: rotor position control} +0 ! PA_Mode - Pitch actuator mode {0 - not used, 1 - first order filter, 2 - second order filter} +0 ! PF_Mode - Pitch fault mode {0 - not used, 1 - constant offset on one or more blades} +0 ! AWC_Mode - Active wake control {0 - not used, 1 - complex number method, 2 - Coleman transform method} +0 ! Ext_Mode - External control mode {0 - not used, 1 - call external dynamic library} +1 ! ZMQ_Mode - Fuse ZeroMQ interface {0: unused, 1: Yaw Control} +0 ! CC_Mode - Cable control mode [0- unused, 1- User defined, 2- Open loop control] +0 ! StC_Mode - Structural control mode [0- unused, 1- User defined, 2- Open loop control] + +!------- FILTERS ---------------------------------------------------------- +1.57080 ! F_LPFCornerFreq - Corner frequency (-3dB point) in the low-pass filters, [rad/s] +0.00000 ! F_LPFDamping - Damping coefficient {used only when F_FilterType = 2} [-] +0 ! F_NumNotchFilts - Number of notch filters placed on sensors +0.0000 ! F_NotchFreqs - Natural frequency of the notch filters. Array with length F_NumNotchFilts +0.0000 ! F_NotchBetaNum - Damping value of numerator (determines the width of notch). Array with length F_NumNotchFilts, [-] +0.0000 ! F_NotchBetaDen - Damping value of denominator (determines the depth of notch). Array with length F_NumNotchFilts, [-] +0 ! F_GenSpdNotch_N - Number of notch filters on generator speed +0 ! F_GenSpdNotch_Ind - Indices of notch filters on generator speed +0 ! F_TwrTopNotch_N - Number of notch filters on tower top acceleration signal +0 ! F_TwrTopNotch_Ind - Indices of notch filters on tower top acceleration signal +0.62830 ! F_SSCornerFreq - Corner frequency (-3dB point) in the first order low pass filter for the setpoint smoother, [rad/s]. +0.20944 ! F_WECornerFreq - Corner frequency (-3dB point) in the first order low pass filter for the wind speed estimate [rad/s]. +0.17952 ! F_YawErr - Low pass filter corner frequency for yaw controller [rad/s]. +0.000000 1.000000 ! F_FlCornerFreq - Natural frequency and damping in the second order low pass filter of the tower-top fore-aft motion for floating feedback control [rad/s, -]. +0.01042 ! F_FlHighPassFreq - Natural frequency of first-order high-pass filter for nacelle fore-aft motion [rad/s]. +0.0000 1.0000 ! F_FlpCornerFreq - Corner frequency and damping in the second order low pass filter of the blade root bending moment for flap control + +!------- BLADE PITCH CONTROL ---------------------------------------------- +30 ! PC_GS_n - Amount of gain-scheduling table entries +0.056789 0.084492 0.106018 0.124332 0.140807 0.155903 0.169931 0.183270 0.196062 0.208354 0.220050 0.231503 0.242646 0.253377 0.263967 0.274233 0.284343 0.294292 0.303997 0.313626 0.322957 0.332260 0.341319 0.350368 0.359221 0.368059 0.376700 0.385301 0.393691 0.402050 ! PC_GS_angles - Gain-schedule table: pitch angles [rad]. +-0.019085 -0.016739 -0.014837 -0.013265 -0.011943 -0.010816 -0.009844 -0.008997 -0.008252 -0.007593 -0.007004 -0.006475 -0.005998 -0.005565 -0.005171 -0.004810 -0.004479 -0.004173 -0.003890 -0.003628 -0.003385 -0.003157 -0.002945 -0.002746 -0.002559 -0.002384 -0.002219 -0.002062 -0.001915 -0.001775 ! PC_GS_KP - Gain-schedule table: pitch controller kp gains [s]. +-0.008417 -0.007536 -0.006822 -0.006232 -0.005735 -0.005312 -0.004947 -0.004629 -0.004350 -0.004102 -0.003881 -0.003682 -0.003503 -0.003341 -0.003192 -0.003057 -0.002932 -0.002818 -0.002712 -0.002613 -0.002522 -0.002436 -0.002357 -0.002282 -0.002212 -0.002146 -0.002084 -0.002025 -0.001970 -0.001917 ! PC_GS_KI - Gain-schedule table: pitch controller ki gains [-]. +0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 ! PC_GS_KD - Gain-schedule table: pitch controller kd gains +0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 ! PC_GS_TF - Gain-schedule table: pitch controller tf gains (derivative filter) +1.570000000000 ! PC_MaxPit - Maximum physical pitch limit, [rad]. +0.000880000000 ! PC_MinPit - Minimum physical pitch limit, [rad]. +0.174500000000 ! PC_MaxRat - Maximum pitch rate (in absolute value) in pitch controller, [rad/s]. +-0.17450000000 ! PC_MinRat - Minimum pitch rate (in absolute value) in pitch controller, [rad/s]. +122.9096700000 ! PC_RefSpd - Desired (reference) HSS speed for pitch controller, [rad/s]. +0.000880000000 ! PC_FinePit - Record 5: Below-rated pitch angle set-point, [rad] +0.017450000000 ! PC_Switch - Angle above lowest minimum pitch angle for switch, [rad] + +!------- INDIVIDUAL PITCH CONTROL ----------------------------------------- +9.120000 11.400000 ! IPC_Vramp - Start and end wind speeds for cut-in ramp function. First entry: IPC inactive, second entry: IPC fully active. [m/s] +2 ! IPC_SatMode - IPC Saturation method (0 - no saturation (except by PC_MinPit), 1 - saturate by PS_BldPitchMin, 2 - saturate sotfly (full IPC cycle) by PC_MinPit, 3 - saturate softly by PS_BldPitchMin) +0.3 ! IPC_IntSat - Integrator saturation (maximum signal amplitude contribution to pitch from IPC), [rad] +0.000e+00 0.000e+00 ! IPC_KP - Proportional gain for the individual pitch controller: first parameter for 1P reductions, second for 2P reductions, [-] +0.000e+00 0.000e+00 ! IPC_KI - Integral gain for the individual pitch controller: first parameter for 1P reductions, second for 2P reductions, [-] +0.000000 0.000000 ! IPC_aziOffset - Phase offset added to the azimuth angle for the individual pitch controller, [rad]. +0.0 ! IPC_CornerFreqAct - Corner frequency of the first-order actuators model, to induce a phase lag in the IPC signal {0: Disable}, [rad/s] + +!------- VS TORQUE CONTROL ------------------------------------------------ +94.40000000000 ! VS_GenEff - Generator efficiency mechanical power -> electrical power, [should match the efficiency defined in the generator properties!], [%] +43093.51876000 ! VS_ArSatTq - Above rated generator torque PI control saturation, [Nm] +40000.00000000 ! VS_MaxRat - Maximum torque rate (in absolute value) in torque controller, [Nm/s]. +47402.87063000 ! VS_MaxTq - Maximum generator torque in Region 3 (HSS side), [Nm]. +0.000000000000 ! VS_MinTq - Minimum generator torque (HSS side), [Nm]. +35.29006000000 ! VS_MinOMSpd - Minimum generator speed [rad/s] +2.063350000000 ! VS_Rgn2K - Generator torque constant in Region 2 (HSS side). Only used in VS_ControlMode = 1,3 +5000000.000000 ! VS_RtPwr - Wind turbine rated power [W] +43093.51876000 ! VS_RtTq - Rated torque, [Nm]. +122.9096700000 ! VS_RefSpd - Rated generator speed [rad/s] +1 ! VS_n - Number of generator PI torque controller gains +-654.312360000 ! VS_KP - Proportional gain for generator PI torque controller [-]. (Only used in the transitional 2.5 region if VS_ControlMode =/ 2) +-104.507080000 ! VS_KI - Integral gain for generator PI torque controller [s]. (Only used in the transitional 2.5 region if VS_ControlMode =/ 2) +7.64 ! VS_TSRopt - Power-maximizing region 2 tip-speed-ratio. Only used in VS_ControlMode = 2. +0.314000000000 ! VS_PwrFiltF - Low pass filter on power used to determine generator speed set point. Only used in VS_ControlMode = 3. + +!------- SETPOINT SMOOTHER --------------------------------------------- +1.00000 ! SS_VSGain - Variable speed torque controller setpoint smoother gain, [-]. +0.00100 ! SS_PCGain - Collective pitch controller setpoint smoother gain, [-]. + +!------- POWER REFERENCE TRACKING -------------------------------------- +2 ! PRC_n - Number of elements in PRC_WindSpeeds and PRC_GenSpeeds array +0.07854 ! PRC_LPF_Freq - Frequency of the low pass filter on the wind speed estimate used to set PRC_GenSpeeds [rad/s] +3.0000 25.0000 ! PRC_WindSpeeds - Array of wind speeds used in rotor speed vs. wind speed lookup table [m/s] +0.7917 0.7917 ! PRC_GenSpeeds - Array of generator speeds corresponding to PRC_WindSpeeds [rad/s] + +!------- WIND SPEED ESTIMATOR --------------------------------------------- +63.000 ! WE_BladeRadius - Blade length (distance from hub center to blade tip), [m] +1 ! WE_CP_n - Amount of parameters in the Cp array +0.0 ! WE_CP - Parameters that define the parameterized CP(lambda) function +0.0 ! WE_Gamma - Adaption gain of the wind speed estimator algorithm [m/rad] +97.0 ! WE_GearboxRatio - Gearbox ratio [>=1], [-] +43702538.05700 ! WE_Jtot - Total drivetrain inertia, including blades, hub and casted generator inertia to LSS, [kg m^2] +1.225 ! WE_RhoAir - Air density, [kg m^-3] +"Cp_Ct_Cq.NREL5MW.txt" ! PerfFileName - File containing rotor performance tables (Cp,Ct,Cq) (absolute path or relative to this file) +36 26 ! PerfTableSize - Size of rotor performance tables, first number refers to number of blade pitch angles, second number referse to number of tip-speed ratios +60 ! WE_FOPoles_N - Number of first-order system poles used in EKF +3.0000 3.2897 3.5793 3.8690 4.1586 4.4483 4.7379 5.0276 5.3172 5.6069 5.8966 6.1862 6.4759 6.7655 7.0552 7.3448 7.6345 7.9241 8.2138 8.5034 8.7931 9.0828 9.3724 9.6621 9.9517 10.2414 10.5310 10.8207 11.1103 11.4000 11.8533 12.3067 12.7600 13.2133 13.6667 14.1200 14.5733 15.0267 15.4800 15.9333 16.3867 16.8400 17.2933 17.7467 18.2000 18.6533 19.1067 19.5600 20.0133 20.4667 20.9200 21.3733 21.8267 22.2800 22.7333 23.1867 23.6400 24.0933 24.5467 25.0000 ! WE_FOPoles_v - Wind speeds corresponding to first-order system poles [m/s] +-0.01640352 -0.01798730 -0.01957109 -0.02115488 -0.02273867 -0.02432245 -0.02590624 -0.02749003 -0.02907382 -0.03065761 -0.03224139 -0.03382518 -0.03540897 -0.03699276 -0.03857654 -0.04016033 -0.04174412 -0.04332791 -0.04491170 -0.04649548 -0.04807927 -0.04966306 -0.05124685 -0.05283063 -0.05441442 -0.05599821 -0.05763347 -0.05907205 -0.06912889 -0.05993737 -0.05021616 -0.05780794 -0.06849544 -0.08052122 -0.09351145 -0.10710432 -0.12106730 -0.13547025 -0.15041833 -0.16588021 -0.18135551 -0.19724989 -0.21342206 -0.22970423 -0.24663982 -0.26354532 -0.28064419 -0.29794214 -0.31532544 -0.33332004 -0.35128130 -0.36985759 -0.38827549 -0.40713466 -0.42584061 -0.44509747 -0.46449375 -0.48460700 -0.50475242 -0.52537402 ! WE_FOPoles - First order system poles [1/s] + +!------- YAW CONTROL ------------------------------------------------------ +0.00000 ! Y_uSwitch - Wind speed to switch between Y_ErrThresh. If zero, only the second value of Y_ErrThresh is used [m/s] +4.000000 8.000000 ! Y_ErrThresh - Yaw error threshold/deadbands. Turbine begins to yaw when it passes this. If Y_uSwitch is zero, only the second value is used. [deg]. +0.00870 ! Y_Rate - Yaw rate [rad/s] +0.00000 ! Y_MErrSet - Integrator saturation (maximum signal amplitude contribution to pitch from yaw-by-IPC), [rad] +0.00000 ! Y_IPC_IntSat - Integrator saturation (maximum signal amplitude contribution to pitch from yaw-by-IPC), [rad] +0.00000 ! Y_IPC_KP - Yaw-by-IPC proportional controller gain Kp +0.00000 ! Y_IPC_KI - Yaw-by-IPC integral controller gain Ki + +!------- TOWER CONTROL ------------------------------------------------------ +0.00000 ! TRA_ExclSpeed - Rotor speed for exclusion [LSS, rad/s] +0.00000 ! TRA_ExclBand - Size of the rotor frequency exclusion band [LSS, rad/s]. Torque controller reference will be TRA_ExclSpeed +/- TRA_ExlBand/2 +0.00000e+00 ! TRA_RateLimit - Rate limit of change in rotor speed reference [LSS, rad/s]. Suggested to be VS_RefSpd/400. +0.00000 ! FA_KI - Integral gain for the fore-aft tower damper controller, [rad*s/m] +0.00000 ! FA_HPFCornerFreq - Corner frequency (-3dB point) in the high-pass filter on the fore-aft acceleration signal [rad/s] +0.00000 ! FA_IntSat - Integrator saturation (maximum signal amplitude contribution to pitch from FA damper), [rad] + +!------- MINIMUM PITCH SATURATION ------------------------------------------- +60 ! PS_BldPitchMin_N - Number of values in minimum blade pitch lookup table (should equal number of values in PS_WindSpeeds and PS_BldPitchMin) +3.000 3.290 3.579 3.869 4.159 4.448 4.738 5.028 5.317 5.607 5.897 6.186 6.476 6.766 7.055 7.345 7.634 7.924 8.214 8.503 8.793 9.083 9.372 9.662 9.952 10.241 10.531 10.821 11.110 11.400 11.853 12.307 12.760 13.213 13.667 14.120 14.573 15.027 15.480 15.933 16.387 16.840 17.293 17.747 18.200 18.653 19.107 19.560 20.013 20.467 20.920 21.373 21.827 22.280 22.733 23.187 23.640 24.093 24.547 25.000 ! PS_WindSpeeds - Wind speeds corresponding to minimum blade pitch angles [m/s] +0.001 0.001 0.001 0.001 0.001 0.001 0.001 0.001 0.001 0.001 0.001 0.001 0.001 0.001 0.001 0.001 0.001 0.001 0.001 0.001 0.001 0.001 0.001 0.001 0.001 0.011 0.023 0.032 0.040 0.047 0.059 0.070 0.081 0.091 0.102 0.112 0.122 0.131 0.141 0.150 0.160 0.169 0.178 0.187 0.196 0.205 0.214 0.223 0.232 0.240 0.249 0.257 0.266 0.274 0.282 0.290 0.299 0.307 0.315 0.323 ! PS_BldPitchMin - Minimum blade pitch angles [rad] + +!------- SHUTDOWN ----------------------------------------------------------- +0.436300000000 ! SD_MaxPit - Maximum blade pitch angle to initiate shutdown, [rad] +0.418880000000 ! SD_CornerFreq - Cutoff Frequency for first order low-pass filter for blade pitch angle, [rad/s] + +!------- Floating ----------------------------------------------------------- +1 ! Fl_n - Number of Fl_Kp gains in gain scheduling, optional with default of 1 +0.0000 ! Fl_Kp - Nacelle velocity proportional feedback gain [s] +0.0000 ! Fl_U - Wind speeds for scheduling Fl_Kp, optional if Fl_Kp is single value [m/s] + +!------- FLAP ACTUATION ----------------------------------------------------- +0.000000000000 ! Flp_Angle - Initial or steady state flap angle [rad] +0.00000000e+00 ! Flp_Kp - Blade root bending moment proportional gain for flap control [s] +0.00000000e+00 ! Flp_Ki - Flap displacement integral gain for flap control [-] +0.174500000000 ! Flp_MaxPit - Maximum (and minimum) flap pitch angle [rad] + +!------- Open Loop Control ----------------------------------------------------- +"unused" ! OL_Filename - Input file with open loop timeseries (absolute path or relative to this file) +0 ! Ind_Breakpoint - The column in OL_Filename that contains the breakpoint (time if OL_Mode = 1) + 0 0 0 ! Ind_BldPitch - The columns in OL_Filename that contains the blade pitch (1,2,3) inputs in rad [array] +0 ! Ind_GenTq - The column in OL_Filename that contains the generator torque in Nm +0 ! Ind_YawRate - The column in OL_Filename that contains the yaw rate in rad/s +0 ! Ind_Azimuth - The column in OL_Filename that contains the desired azimuth position in rad (used if OL_Mode = 2) +0.0000 0.0000 0.0000 0.0000 ! RP_Gains - PID gains and Tf of derivative for rotor position control (used if OL_Mode = 2) +0 ! Ind_CableControl - The column(s) in OL_Filename that contains the cable control inputs in m [Used with CC_Mode = 2, must be the same size as CC_Group_N] +0 ! Ind_StructControl - The column(s) in OL_Filename that contains the structural control inputs [Used with StC_Mode = 2, must be the same size as StC_Group_N] + +!------- Pitch Actuator Model ----------------------------------------------------- +3.140000000000 ! PA_CornerFreq - Pitch actuator bandwidth/cut-off frequency [rad/s] +0.707000000000 ! PA_Damping - Pitch actuator damping ratio [-, unused if PA_Mode = 1] + +!------- Pitch Actuator Faults ----------------------------------------------------- +0.00000000 0.00000000 0.00000000 ! PF_Offsets - Constant blade pitch offsets for blades 1-3 [rad] + +!------- Active Wake Control ----------------------------------------------------- +1 ! AWC_NumModes - Number of user-defined AWC forcing modes +1 ! AWC_n - Azimuthal mode number(s) (i.e., the number and direction of the lobes of the wake structure) +1 ! AWC_harmonic - Harmonic(s) to apply in the AWC Inverse Coleman Transformation (only used when AWC_Mode = 2) +0.0500 ! AWC_freq - Frequency(s) of forcing mode(s) [Hz] +1.0000 ! AWC_amp - Pitch amplitude(s) of individual forcing mode(s) [deg] +0.0000 ! AWC_clockangle - Initial angle(s) of forcing mode(s) [deg] + +!------- External Controller Interface ----------------------------------------------------- +"unused" ! DLL_FileName - Name/location of the dynamic library in the Bladed-DLL format +"unused" ! DLL_InFile - Name of input file sent to the DLL (-) +"DISCON" ! DLL_ProcName - Name of procedure in DLL to be called (-) + +!------- ZeroMQ Interface --------------------------------------------------------- +"tcp://localhost:5556" ! ZMQ_CommAddress - Communication address for ZMQ server, (e.g. "tcp://localhost:5555") +1.000000 ! ZMQ_UpdatePeriod - Update period at zmq interface to send measurements and wait for setpoint [sec.] +0 ! ZMQ_ID - Integer identifier of turbine + +!------- Cable Control --------------------------------------------------------- +1 ! CC_Group_N - Number of cable control groups +0 ! CC_GroupIndex - First index for cable control group, should correspond to deltaL +20.000000 ! CC_ActTau - Time constant for line actuator [s] + +!------- Structural Controllers --------------------------------------------------------- +1 ! StC_Group_N - Number of cable control groups +0 ! StC_GroupIndex - First index for structural control group, options specified in ServoDyn summary output diff --git a/examples/FAST.Farm_interface/inputs/FFFiles/DISCON_WT2.IN b/examples/FAST.Farm_interface/inputs/FFFiles/DISCON_WT2.IN new file mode 100644 index 00000000..d93420e6 --- /dev/null +++ b/examples/FAST.Farm_interface/inputs/FFFiles/DISCON_WT2.IN @@ -0,0 +1,198 @@ +! Controller parameter input file for the FAST.Farm wind turbine +! - File written using ROSCO version 2.9.4 controller tuning logic on 10/11/25 + +!------- SIMULATION CONTROL ------------------------------------------------------------ +1 ! LoggingLevel - {0: write no debug files, 1: write standard output .dbg-file, 2: LoggingLevel 1 + ROSCO LocalVars (.dbg2) 3: LoggingLevel 2 + complete avrSWAP-array (.dbg3)} +0.0 ! DT_Out - {Time step to output .dbg* files, or 0 to match sampling period of OpenFAST} +1 ! Ext_Interface - (0 - use standard bladed interface, 1 - Use the extened DLL interface introduced in OpenFAST 3.5.0.) +0 ! Echo - (0 - no Echo, 1 - Echo input data to .echo) + +!------- CONTROLLER FLAGS ------------------------------------------------- +1 ! F_LPFType - (1: first-order low-pass filter, 2: second-order low-pass filter), [rad/s] (currently filters generator speed and pitch control signals +0 ! IPC_ControlMode - Turn Individual Pitch Control (IPC) for fatigue load reductions (pitch contribution) {0: off, 1: 1P reductions, 2: 1P+2P reductions} +3 ! VS_ControlMode - Generator torque control mode in above rated conditions (0- no torque control, 1- k*omega^2 with PI transitions, 2- WSE TSR Tracking, 3- Power-based TSR Tracking)} +0 ! VS_ConstPower - Do constant power torque control, where above rated torque varies, 0 for constant torque} +1 ! PC_ControlMode - Blade pitch control mode {0: No pitch, fix to fine pitch, 1: active PI blade pitch control} +0 ! Y_ControlMode - Yaw control mode {0: no yaw control, 1: yaw rate control, 2: yaw-by-IPC} +1 ! SS_Mode - Setpoint Smoother mode {0: no setpoint smoothing, 1: introduce setpoint smoothing} +0 ! PRC_Mode - Power reference tracking mode{0: use standard rotor speed set points, 1: use PRC rotor speed setpoints} +2 ! WE_Mode - Wind speed estimator mode {0: One-second low pass filtered hub height wind speed, 1: Immersion and Invariance Estimator, 2: Extended Kalman Filter} +1 ! PS_Mode - Pitch saturation mode {0: no pitch saturation, 1: implement pitch saturation} +0 ! SD_Mode - Shutdown mode {0: no shutdown procedure, 1: pitch to max pitch at shutdown} +0 ! Fl_Mode - Floating specific feedback mode {0: no nacelle velocity feedback, 1: feed back translational velocity, 2: feed back rotational veloicty} +0 ! TD_Mode - Tower damper mode (0- no tower damper, 1- feed back translational nacelle accelleration to pitch angle +0 ! TRA_Mode - Tower resonance avoidance mode (0- no tower resonsnace avoidance, 1- use torque control setpoints to avoid a specific frequency +0 ! Flp_Mode - Flap control mode {0: no flap control, 1: steady state flap angle, 2: Proportional flap control, 2: Cyclic (1P) flap control} +0 ! OL_Mode - Open loop control mode {0: no open loop control, 1: open loop control vs. time, 2: rotor position control} +0 ! PA_Mode - Pitch actuator mode {0 - not used, 1 - first order filter, 2 - second order filter} +0 ! PF_Mode - Pitch fault mode {0 - not used, 1 - constant offset on one or more blades} +0 ! AWC_Mode - Active wake control {0 - not used, 1 - complex number method, 2 - Coleman transform method} +0 ! Ext_Mode - External control mode {0 - not used, 1 - call external dynamic library} +1 ! ZMQ_Mode - Fuse ZeroMQ interface {0: unused, 1: Yaw Control} +0 ! CC_Mode - Cable control mode [0- unused, 1- User defined, 2- Open loop control] +0 ! StC_Mode - Structural control mode [0- unused, 1- User defined, 2- Open loop control] + +!------- FILTERS ---------------------------------------------------------- +1.57080 ! F_LPFCornerFreq - Corner frequency (-3dB point) in the low-pass filters, [rad/s] +0.00000 ! F_LPFDamping - Damping coefficient {used only when F_FilterType = 2} [-] +0 ! F_NumNotchFilts - Number of notch filters placed on sensors +0.0000 ! F_NotchFreqs - Natural frequency of the notch filters. Array with length F_NumNotchFilts +0.0000 ! F_NotchBetaNum - Damping value of numerator (determines the width of notch). Array with length F_NumNotchFilts, [-] +0.0000 ! F_NotchBetaDen - Damping value of denominator (determines the depth of notch). Array with length F_NumNotchFilts, [-] +0 ! F_GenSpdNotch_N - Number of notch filters on generator speed +0 ! F_GenSpdNotch_Ind - Indices of notch filters on generator speed +0 ! F_TwrTopNotch_N - Number of notch filters on tower top acceleration signal +0 ! F_TwrTopNotch_Ind - Indices of notch filters on tower top acceleration signal +0.62830 ! F_SSCornerFreq - Corner frequency (-3dB point) in the first order low pass filter for the setpoint smoother, [rad/s]. +0.20944 ! F_WECornerFreq - Corner frequency (-3dB point) in the first order low pass filter for the wind speed estimate [rad/s]. +0.17952 ! F_YawErr - Low pass filter corner frequency for yaw controller [rad/s]. +0.000000 1.000000 ! F_FlCornerFreq - Natural frequency and damping in the second order low pass filter of the tower-top fore-aft motion for floating feedback control [rad/s, -]. +0.01042 ! F_FlHighPassFreq - Natural frequency of first-order high-pass filter for nacelle fore-aft motion [rad/s]. +0.0000 1.0000 ! F_FlpCornerFreq - Corner frequency and damping in the second order low pass filter of the blade root bending moment for flap control + +!------- BLADE PITCH CONTROL ---------------------------------------------- +30 ! PC_GS_n - Amount of gain-scheduling table entries +0.056789 0.084492 0.106018 0.124332 0.140807 0.155903 0.169931 0.183270 0.196062 0.208354 0.220050 0.231503 0.242646 0.253377 0.263967 0.274233 0.284343 0.294292 0.303997 0.313626 0.322957 0.332260 0.341319 0.350368 0.359221 0.368059 0.376700 0.385301 0.393691 0.402050 ! PC_GS_angles - Gain-schedule table: pitch angles [rad]. +-0.019085 -0.016739 -0.014837 -0.013265 -0.011943 -0.010816 -0.009844 -0.008997 -0.008252 -0.007593 -0.007004 -0.006475 -0.005998 -0.005565 -0.005171 -0.004810 -0.004479 -0.004173 -0.003890 -0.003628 -0.003385 -0.003157 -0.002945 -0.002746 -0.002559 -0.002384 -0.002219 -0.002062 -0.001915 -0.001775 ! PC_GS_KP - Gain-schedule table: pitch controller kp gains [s]. +-0.008417 -0.007536 -0.006822 -0.006232 -0.005735 -0.005312 -0.004947 -0.004629 -0.004350 -0.004102 -0.003881 -0.003682 -0.003503 -0.003341 -0.003192 -0.003057 -0.002932 -0.002818 -0.002712 -0.002613 -0.002522 -0.002436 -0.002357 -0.002282 -0.002212 -0.002146 -0.002084 -0.002025 -0.001970 -0.001917 ! PC_GS_KI - Gain-schedule table: pitch controller ki gains [-]. +0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 ! PC_GS_KD - Gain-schedule table: pitch controller kd gains +0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 ! PC_GS_TF - Gain-schedule table: pitch controller tf gains (derivative filter) +1.570000000000 ! PC_MaxPit - Maximum physical pitch limit, [rad]. +0.000880000000 ! PC_MinPit - Minimum physical pitch limit, [rad]. +0.174500000000 ! PC_MaxRat - Maximum pitch rate (in absolute value) in pitch controller, [rad/s]. +-0.17450000000 ! PC_MinRat - Minimum pitch rate (in absolute value) in pitch controller, [rad/s]. +122.9096700000 ! PC_RefSpd - Desired (reference) HSS speed for pitch controller, [rad/s]. +0.000880000000 ! PC_FinePit - Record 5: Below-rated pitch angle set-point, [rad] +0.017450000000 ! PC_Switch - Angle above lowest minimum pitch angle for switch, [rad] + +!------- INDIVIDUAL PITCH CONTROL ----------------------------------------- +9.120000 11.400000 ! IPC_Vramp - Start and end wind speeds for cut-in ramp function. First entry: IPC inactive, second entry: IPC fully active. [m/s] +2 ! IPC_SatMode - IPC Saturation method (0 - no saturation (except by PC_MinPit), 1 - saturate by PS_BldPitchMin, 2 - saturate sotfly (full IPC cycle) by PC_MinPit, 3 - saturate softly by PS_BldPitchMin) +0.3 ! IPC_IntSat - Integrator saturation (maximum signal amplitude contribution to pitch from IPC), [rad] +0.000e+00 0.000e+00 ! IPC_KP - Proportional gain for the individual pitch controller: first parameter for 1P reductions, second for 2P reductions, [-] +0.000e+00 0.000e+00 ! IPC_KI - Integral gain for the individual pitch controller: first parameter for 1P reductions, second for 2P reductions, [-] +0.000000 0.000000 ! IPC_aziOffset - Phase offset added to the azimuth angle for the individual pitch controller, [rad]. +0.0 ! IPC_CornerFreqAct - Corner frequency of the first-order actuators model, to induce a phase lag in the IPC signal {0: Disable}, [rad/s] + +!------- VS TORQUE CONTROL ------------------------------------------------ +94.40000000000 ! VS_GenEff - Generator efficiency mechanical power -> electrical power, [should match the efficiency defined in the generator properties!], [%] +43093.51876000 ! VS_ArSatTq - Above rated generator torque PI control saturation, [Nm] +40000.00000000 ! VS_MaxRat - Maximum torque rate (in absolute value) in torque controller, [Nm/s]. +47402.87063000 ! VS_MaxTq - Maximum generator torque in Region 3 (HSS side), [Nm]. +0.000000000000 ! VS_MinTq - Minimum generator torque (HSS side), [Nm]. +35.29006000000 ! VS_MinOMSpd - Minimum generator speed [rad/s] +2.063350000000 ! VS_Rgn2K - Generator torque constant in Region 2 (HSS side). Only used in VS_ControlMode = 1,3 +5000000.000000 ! VS_RtPwr - Wind turbine rated power [W] +43093.51876000 ! VS_RtTq - Rated torque, [Nm]. +122.9096700000 ! VS_RefSpd - Rated generator speed [rad/s] +1 ! VS_n - Number of generator PI torque controller gains +-654.312360000 ! VS_KP - Proportional gain for generator PI torque controller [-]. (Only used in the transitional 2.5 region if VS_ControlMode =/ 2) +-104.507080000 ! VS_KI - Integral gain for generator PI torque controller [s]. (Only used in the transitional 2.5 region if VS_ControlMode =/ 2) +7.64 ! VS_TSRopt - Power-maximizing region 2 tip-speed-ratio. Only used in VS_ControlMode = 2. +0.314000000000 ! VS_PwrFiltF - Low pass filter on power used to determine generator speed set point. Only used in VS_ControlMode = 3. + +!------- SETPOINT SMOOTHER --------------------------------------------- +1.00000 ! SS_VSGain - Variable speed torque controller setpoint smoother gain, [-]. +0.00100 ! SS_PCGain - Collective pitch controller setpoint smoother gain, [-]. + +!------- POWER REFERENCE TRACKING -------------------------------------- +2 ! PRC_n - Number of elements in PRC_WindSpeeds and PRC_GenSpeeds array +0.07854 ! PRC_LPF_Freq - Frequency of the low pass filter on the wind speed estimate used to set PRC_GenSpeeds [rad/s] +3.0000 25.0000 ! PRC_WindSpeeds - Array of wind speeds used in rotor speed vs. wind speed lookup table [m/s] +0.7917 0.7917 ! PRC_GenSpeeds - Array of generator speeds corresponding to PRC_WindSpeeds [rad/s] + +!------- WIND SPEED ESTIMATOR --------------------------------------------- +63.000 ! WE_BladeRadius - Blade length (distance from hub center to blade tip), [m] +1 ! WE_CP_n - Amount of parameters in the Cp array +0.0 ! WE_CP - Parameters that define the parameterized CP(lambda) function +0.0 ! WE_Gamma - Adaption gain of the wind speed estimator algorithm [m/rad] +97.0 ! WE_GearboxRatio - Gearbox ratio [>=1], [-] +43702538.05700 ! WE_Jtot - Total drivetrain inertia, including blades, hub and casted generator inertia to LSS, [kg m^2] +1.225 ! WE_RhoAir - Air density, [kg m^-3] +"Cp_Ct_Cq.NREL5MW.txt" ! PerfFileName - File containing rotor performance tables (Cp,Ct,Cq) (absolute path or relative to this file) +36 26 ! PerfTableSize - Size of rotor performance tables, first number refers to number of blade pitch angles, second number referse to number of tip-speed ratios +60 ! WE_FOPoles_N - Number of first-order system poles used in EKF +3.0000 3.2897 3.5793 3.8690 4.1586 4.4483 4.7379 5.0276 5.3172 5.6069 5.8966 6.1862 6.4759 6.7655 7.0552 7.3448 7.6345 7.9241 8.2138 8.5034 8.7931 9.0828 9.3724 9.6621 9.9517 10.2414 10.5310 10.8207 11.1103 11.4000 11.8533 12.3067 12.7600 13.2133 13.6667 14.1200 14.5733 15.0267 15.4800 15.9333 16.3867 16.8400 17.2933 17.7467 18.2000 18.6533 19.1067 19.5600 20.0133 20.4667 20.9200 21.3733 21.8267 22.2800 22.7333 23.1867 23.6400 24.0933 24.5467 25.0000 ! WE_FOPoles_v - Wind speeds corresponding to first-order system poles [m/s] +-0.01640352 -0.01798730 -0.01957109 -0.02115488 -0.02273867 -0.02432245 -0.02590624 -0.02749003 -0.02907382 -0.03065761 -0.03224139 -0.03382518 -0.03540897 -0.03699276 -0.03857654 -0.04016033 -0.04174412 -0.04332791 -0.04491170 -0.04649548 -0.04807927 -0.04966306 -0.05124685 -0.05283063 -0.05441442 -0.05599821 -0.05763347 -0.05907205 -0.06912889 -0.05993737 -0.05021616 -0.05780794 -0.06849544 -0.08052122 -0.09351145 -0.10710432 -0.12106730 -0.13547025 -0.15041833 -0.16588021 -0.18135551 -0.19724989 -0.21342206 -0.22970423 -0.24663982 -0.26354532 -0.28064419 -0.29794214 -0.31532544 -0.33332004 -0.35128130 -0.36985759 -0.38827549 -0.40713466 -0.42584061 -0.44509747 -0.46449375 -0.48460700 -0.50475242 -0.52537402 ! WE_FOPoles - First order system poles [1/s] + +!------- YAW CONTROL ------------------------------------------------------ +0.00000 ! Y_uSwitch - Wind speed to switch between Y_ErrThresh. If zero, only the second value of Y_ErrThresh is used [m/s] +4.000000 8.000000 ! Y_ErrThresh - Yaw error threshold/deadbands. Turbine begins to yaw when it passes this. If Y_uSwitch is zero, only the second value is used. [deg]. +0.00870 ! Y_Rate - Yaw rate [rad/s] +0.00000 ! Y_MErrSet - Integrator saturation (maximum signal amplitude contribution to pitch from yaw-by-IPC), [rad] +0.00000 ! Y_IPC_IntSat - Integrator saturation (maximum signal amplitude contribution to pitch from yaw-by-IPC), [rad] +0.00000 ! Y_IPC_KP - Yaw-by-IPC proportional controller gain Kp +0.00000 ! Y_IPC_KI - Yaw-by-IPC integral controller gain Ki + +!------- TOWER CONTROL ------------------------------------------------------ +0.00000 ! TRA_ExclSpeed - Rotor speed for exclusion [LSS, rad/s] +0.00000 ! TRA_ExclBand - Size of the rotor frequency exclusion band [LSS, rad/s]. Torque controller reference will be TRA_ExclSpeed +/- TRA_ExlBand/2 +0.00000e+00 ! TRA_RateLimit - Rate limit of change in rotor speed reference [LSS, rad/s]. Suggested to be VS_RefSpd/400. +0.00000 ! FA_KI - Integral gain for the fore-aft tower damper controller, [rad*s/m] +0.00000 ! FA_HPFCornerFreq - Corner frequency (-3dB point) in the high-pass filter on the fore-aft acceleration signal [rad/s] +0.00000 ! FA_IntSat - Integrator saturation (maximum signal amplitude contribution to pitch from FA damper), [rad] + +!------- MINIMUM PITCH SATURATION ------------------------------------------- +60 ! PS_BldPitchMin_N - Number of values in minimum blade pitch lookup table (should equal number of values in PS_WindSpeeds and PS_BldPitchMin) +3.000 3.290 3.579 3.869 4.159 4.448 4.738 5.028 5.317 5.607 5.897 6.186 6.476 6.766 7.055 7.345 7.634 7.924 8.214 8.503 8.793 9.083 9.372 9.662 9.952 10.241 10.531 10.821 11.110 11.400 11.853 12.307 12.760 13.213 13.667 14.120 14.573 15.027 15.480 15.933 16.387 16.840 17.293 17.747 18.200 18.653 19.107 19.560 20.013 20.467 20.920 21.373 21.827 22.280 22.733 23.187 23.640 24.093 24.547 25.000 ! PS_WindSpeeds - Wind speeds corresponding to minimum blade pitch angles [m/s] +0.001 0.001 0.001 0.001 0.001 0.001 0.001 0.001 0.001 0.001 0.001 0.001 0.001 0.001 0.001 0.001 0.001 0.001 0.001 0.001 0.001 0.001 0.001 0.001 0.001 0.011 0.023 0.032 0.040 0.047 0.059 0.070 0.081 0.091 0.102 0.112 0.122 0.131 0.141 0.150 0.160 0.169 0.178 0.187 0.196 0.205 0.214 0.223 0.232 0.240 0.249 0.257 0.266 0.274 0.282 0.290 0.299 0.307 0.315 0.323 ! PS_BldPitchMin - Minimum blade pitch angles [rad] + +!------- SHUTDOWN ----------------------------------------------------------- +0.436300000000 ! SD_MaxPit - Maximum blade pitch angle to initiate shutdown, [rad] +0.418880000000 ! SD_CornerFreq - Cutoff Frequency for first order low-pass filter for blade pitch angle, [rad/s] + +!------- Floating ----------------------------------------------------------- +1 ! Fl_n - Number of Fl_Kp gains in gain scheduling, optional with default of 1 +0.0000 ! Fl_Kp - Nacelle velocity proportional feedback gain [s] +0.0000 ! Fl_U - Wind speeds for scheduling Fl_Kp, optional if Fl_Kp is single value [m/s] + +!------- FLAP ACTUATION ----------------------------------------------------- +0.000000000000 ! Flp_Angle - Initial or steady state flap angle [rad] +0.00000000e+00 ! Flp_Kp - Blade root bending moment proportional gain for flap control [s] +0.00000000e+00 ! Flp_Ki - Flap displacement integral gain for flap control [-] +0.174500000000 ! Flp_MaxPit - Maximum (and minimum) flap pitch angle [rad] + +!------- Open Loop Control ----------------------------------------------------- +"unused" ! OL_Filename - Input file with open loop timeseries (absolute path or relative to this file) +0 ! Ind_Breakpoint - The column in OL_Filename that contains the breakpoint (time if OL_Mode = 1) + 0 0 0 ! Ind_BldPitch - The columns in OL_Filename that contains the blade pitch (1,2,3) inputs in rad [array] +0 ! Ind_GenTq - The column in OL_Filename that contains the generator torque in Nm +0 ! Ind_YawRate - The column in OL_Filename that contains the yaw rate in rad/s +0 ! Ind_Azimuth - The column in OL_Filename that contains the desired azimuth position in rad (used if OL_Mode = 2) +0.0000 0.0000 0.0000 0.0000 ! RP_Gains - PID gains and Tf of derivative for rotor position control (used if OL_Mode = 2) +0 ! Ind_CableControl - The column(s) in OL_Filename that contains the cable control inputs in m [Used with CC_Mode = 2, must be the same size as CC_Group_N] +0 ! Ind_StructControl - The column(s) in OL_Filename that contains the structural control inputs [Used with StC_Mode = 2, must be the same size as StC_Group_N] + +!------- Pitch Actuator Model ----------------------------------------------------- +3.140000000000 ! PA_CornerFreq - Pitch actuator bandwidth/cut-off frequency [rad/s] +0.707000000000 ! PA_Damping - Pitch actuator damping ratio [-, unused if PA_Mode = 1] + +!------- Pitch Actuator Faults ----------------------------------------------------- +0.00000000 0.00000000 0.00000000 ! PF_Offsets - Constant blade pitch offsets for blades 1-3 [rad] + +!------- Active Wake Control ----------------------------------------------------- +1 ! AWC_NumModes - Number of user-defined AWC forcing modes +1 ! AWC_n - Azimuthal mode number(s) (i.e., the number and direction of the lobes of the wake structure) +1 ! AWC_harmonic - Harmonic(s) to apply in the AWC Inverse Coleman Transformation (only used when AWC_Mode = 2) +0.0500 ! AWC_freq - Frequency(s) of forcing mode(s) [Hz] +1.0000 ! AWC_amp - Pitch amplitude(s) of individual forcing mode(s) [deg] +0.0000 ! AWC_clockangle - Initial angle(s) of forcing mode(s) [deg] + +!------- External Controller Interface ----------------------------------------------------- +"unused" ! DLL_FileName - Name/location of the dynamic library in the Bladed-DLL format +"unused" ! DLL_InFile - Name of input file sent to the DLL (-) +"DISCON" ! DLL_ProcName - Name of procedure in DLL to be called (-) + +!------- ZeroMQ Interface --------------------------------------------------------- +"tcp://localhost:5556" ! ZMQ_CommAddress - Communication address for ZMQ server, (e.g. "tcp://localhost:5555") +1.000000 ! ZMQ_UpdatePeriod - Update period at zmq interface to send measurements and wait for setpoint [sec.] +1 ! ZMQ_ID - Integer identifier of turbine + +!------- Cable Control --------------------------------------------------------- +1 ! CC_Group_N - Number of cable control groups +0 ! CC_GroupIndex - First index for cable control group, should correspond to deltaL +20.000000 ! CC_ActTau - Time constant for line actuator [s] + +!------- Structural Controllers --------------------------------------------------------- +1 ! StC_Group_N - Number of cable control groups +0 ! StC_GroupIndex - First index for structural control group, options specified in ServoDyn summary output diff --git a/examples/FAST.Farm_interface/inputs/FFFiles/DISCON_WT3.IN b/examples/FAST.Farm_interface/inputs/FFFiles/DISCON_WT3.IN new file mode 100644 index 00000000..0c220e13 --- /dev/null +++ b/examples/FAST.Farm_interface/inputs/FFFiles/DISCON_WT3.IN @@ -0,0 +1,198 @@ +! Controller parameter input file for the FAST.Farm wind turbine +! - File written using ROSCO version 2.9.4 controller tuning logic on 10/11/25 + +!------- SIMULATION CONTROL ------------------------------------------------------------ +1 ! LoggingLevel - {0: write no debug files, 1: write standard output .dbg-file, 2: LoggingLevel 1 + ROSCO LocalVars (.dbg2) 3: LoggingLevel 2 + complete avrSWAP-array (.dbg3)} +0.0 ! DT_Out - {Time step to output .dbg* files, or 0 to match sampling period of OpenFAST} +1 ! Ext_Interface - (0 - use standard bladed interface, 1 - Use the extened DLL interface introduced in OpenFAST 3.5.0.) +0 ! Echo - (0 - no Echo, 1 - Echo input data to .echo) + +!------- CONTROLLER FLAGS ------------------------------------------------- +1 ! F_LPFType - (1: first-order low-pass filter, 2: second-order low-pass filter), [rad/s] (currently filters generator speed and pitch control signals +0 ! IPC_ControlMode - Turn Individual Pitch Control (IPC) for fatigue load reductions (pitch contribution) {0: off, 1: 1P reductions, 2: 1P+2P reductions} +3 ! VS_ControlMode - Generator torque control mode in above rated conditions (0- no torque control, 1- k*omega^2 with PI transitions, 2- WSE TSR Tracking, 3- Power-based TSR Tracking)} +0 ! VS_ConstPower - Do constant power torque control, where above rated torque varies, 0 for constant torque} +1 ! PC_ControlMode - Blade pitch control mode {0: No pitch, fix to fine pitch, 1: active PI blade pitch control} +0 ! Y_ControlMode - Yaw control mode {0: no yaw control, 1: yaw rate control, 2: yaw-by-IPC} +1 ! SS_Mode - Setpoint Smoother mode {0: no setpoint smoothing, 1: introduce setpoint smoothing} +0 ! PRC_Mode - Power reference tracking mode{0: use standard rotor speed set points, 1: use PRC rotor speed setpoints} +2 ! WE_Mode - Wind speed estimator mode {0: One-second low pass filtered hub height wind speed, 1: Immersion and Invariance Estimator, 2: Extended Kalman Filter} +1 ! PS_Mode - Pitch saturation mode {0: no pitch saturation, 1: implement pitch saturation} +0 ! SD_Mode - Shutdown mode {0: no shutdown procedure, 1: pitch to max pitch at shutdown} +0 ! Fl_Mode - Floating specific feedback mode {0: no nacelle velocity feedback, 1: feed back translational velocity, 2: feed back rotational veloicty} +0 ! TD_Mode - Tower damper mode (0- no tower damper, 1- feed back translational nacelle accelleration to pitch angle +0 ! TRA_Mode - Tower resonance avoidance mode (0- no tower resonsnace avoidance, 1- use torque control setpoints to avoid a specific frequency +0 ! Flp_Mode - Flap control mode {0: no flap control, 1: steady state flap angle, 2: Proportional flap control, 2: Cyclic (1P) flap control} +0 ! OL_Mode - Open loop control mode {0: no open loop control, 1: open loop control vs. time, 2: rotor position control} +0 ! PA_Mode - Pitch actuator mode {0 - not used, 1 - first order filter, 2 - second order filter} +0 ! PF_Mode - Pitch fault mode {0 - not used, 1 - constant offset on one or more blades} +0 ! AWC_Mode - Active wake control {0 - not used, 1 - complex number method, 2 - Coleman transform method} +0 ! Ext_Mode - External control mode {0 - not used, 1 - call external dynamic library} +1 ! ZMQ_Mode - Fuse ZeroMQ interface {0: unused, 1: Yaw Control} +0 ! CC_Mode - Cable control mode [0- unused, 1- User defined, 2- Open loop control] +0 ! StC_Mode - Structural control mode [0- unused, 1- User defined, 2- Open loop control] + +!------- FILTERS ---------------------------------------------------------- +1.57080 ! F_LPFCornerFreq - Corner frequency (-3dB point) in the low-pass filters, [rad/s] +0.00000 ! F_LPFDamping - Damping coefficient {used only when F_FilterType = 2} [-] +0 ! F_NumNotchFilts - Number of notch filters placed on sensors +0.0000 ! F_NotchFreqs - Natural frequency of the notch filters. Array with length F_NumNotchFilts +0.0000 ! F_NotchBetaNum - Damping value of numerator (determines the width of notch). Array with length F_NumNotchFilts, [-] +0.0000 ! F_NotchBetaDen - Damping value of denominator (determines the depth of notch). Array with length F_NumNotchFilts, [-] +0 ! F_GenSpdNotch_N - Number of notch filters on generator speed +0 ! F_GenSpdNotch_Ind - Indices of notch filters on generator speed +0 ! F_TwrTopNotch_N - Number of notch filters on tower top acceleration signal +0 ! F_TwrTopNotch_Ind - Indices of notch filters on tower top acceleration signal +0.62830 ! F_SSCornerFreq - Corner frequency (-3dB point) in the first order low pass filter for the setpoint smoother, [rad/s]. +0.20944 ! F_WECornerFreq - Corner frequency (-3dB point) in the first order low pass filter for the wind speed estimate [rad/s]. +0.17952 ! F_YawErr - Low pass filter corner frequency for yaw controller [rad/s]. +0.000000 1.000000 ! F_FlCornerFreq - Natural frequency and damping in the second order low pass filter of the tower-top fore-aft motion for floating feedback control [rad/s, -]. +0.01042 ! F_FlHighPassFreq - Natural frequency of first-order high-pass filter for nacelle fore-aft motion [rad/s]. +0.0000 1.0000 ! F_FlpCornerFreq - Corner frequency and damping in the second order low pass filter of the blade root bending moment for flap control + +!------- BLADE PITCH CONTROL ---------------------------------------------- +30 ! PC_GS_n - Amount of gain-scheduling table entries +0.056789 0.084492 0.106018 0.124332 0.140807 0.155903 0.169931 0.183270 0.196062 0.208354 0.220050 0.231503 0.242646 0.253377 0.263967 0.274233 0.284343 0.294292 0.303997 0.313626 0.322957 0.332260 0.341319 0.350368 0.359221 0.368059 0.376700 0.385301 0.393691 0.402050 ! PC_GS_angles - Gain-schedule table: pitch angles [rad]. +-0.019085 -0.016739 -0.014837 -0.013265 -0.011943 -0.010816 -0.009844 -0.008997 -0.008252 -0.007593 -0.007004 -0.006475 -0.005998 -0.005565 -0.005171 -0.004810 -0.004479 -0.004173 -0.003890 -0.003628 -0.003385 -0.003157 -0.002945 -0.002746 -0.002559 -0.002384 -0.002219 -0.002062 -0.001915 -0.001775 ! PC_GS_KP - Gain-schedule table: pitch controller kp gains [s]. +-0.008417 -0.007536 -0.006822 -0.006232 -0.005735 -0.005312 -0.004947 -0.004629 -0.004350 -0.004102 -0.003881 -0.003682 -0.003503 -0.003341 -0.003192 -0.003057 -0.002932 -0.002818 -0.002712 -0.002613 -0.002522 -0.002436 -0.002357 -0.002282 -0.002212 -0.002146 -0.002084 -0.002025 -0.001970 -0.001917 ! PC_GS_KI - Gain-schedule table: pitch controller ki gains [-]. +0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 ! PC_GS_KD - Gain-schedule table: pitch controller kd gains +0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 ! PC_GS_TF - Gain-schedule table: pitch controller tf gains (derivative filter) +1.570000000000 ! PC_MaxPit - Maximum physical pitch limit, [rad]. +0.000880000000 ! PC_MinPit - Minimum physical pitch limit, [rad]. +0.174500000000 ! PC_MaxRat - Maximum pitch rate (in absolute value) in pitch controller, [rad/s]. +-0.17450000000 ! PC_MinRat - Minimum pitch rate (in absolute value) in pitch controller, [rad/s]. +122.9096700000 ! PC_RefSpd - Desired (reference) HSS speed for pitch controller, [rad/s]. +0.000880000000 ! PC_FinePit - Record 5: Below-rated pitch angle set-point, [rad] +0.017450000000 ! PC_Switch - Angle above lowest minimum pitch angle for switch, [rad] + +!------- INDIVIDUAL PITCH CONTROL ----------------------------------------- +9.120000 11.400000 ! IPC_Vramp - Start and end wind speeds for cut-in ramp function. First entry: IPC inactive, second entry: IPC fully active. [m/s] +2 ! IPC_SatMode - IPC Saturation method (0 - no saturation (except by PC_MinPit), 1 - saturate by PS_BldPitchMin, 2 - saturate sotfly (full IPC cycle) by PC_MinPit, 3 - saturate softly by PS_BldPitchMin) +0.3 ! IPC_IntSat - Integrator saturation (maximum signal amplitude contribution to pitch from IPC), [rad] +0.000e+00 0.000e+00 ! IPC_KP - Proportional gain for the individual pitch controller: first parameter for 1P reductions, second for 2P reductions, [-] +0.000e+00 0.000e+00 ! IPC_KI - Integral gain for the individual pitch controller: first parameter for 1P reductions, second for 2P reductions, [-] +0.000000 0.000000 ! IPC_aziOffset - Phase offset added to the azimuth angle for the individual pitch controller, [rad]. +0.0 ! IPC_CornerFreqAct - Corner frequency of the first-order actuators model, to induce a phase lag in the IPC signal {0: Disable}, [rad/s] + +!------- VS TORQUE CONTROL ------------------------------------------------ +94.40000000000 ! VS_GenEff - Generator efficiency mechanical power -> electrical power, [should match the efficiency defined in the generator properties!], [%] +43093.51876000 ! VS_ArSatTq - Above rated generator torque PI control saturation, [Nm] +40000.00000000 ! VS_MaxRat - Maximum torque rate (in absolute value) in torque controller, [Nm/s]. +47402.87063000 ! VS_MaxTq - Maximum generator torque in Region 3 (HSS side), [Nm]. +0.000000000000 ! VS_MinTq - Minimum generator torque (HSS side), [Nm]. +35.29006000000 ! VS_MinOMSpd - Minimum generator speed [rad/s] +2.063350000000 ! VS_Rgn2K - Generator torque constant in Region 2 (HSS side). Only used in VS_ControlMode = 1,3 +5000000.000000 ! VS_RtPwr - Wind turbine rated power [W] +43093.51876000 ! VS_RtTq - Rated torque, [Nm]. +122.9096700000 ! VS_RefSpd - Rated generator speed [rad/s] +1 ! VS_n - Number of generator PI torque controller gains +-654.312360000 ! VS_KP - Proportional gain for generator PI torque controller [-]. (Only used in the transitional 2.5 region if VS_ControlMode =/ 2) +-104.507080000 ! VS_KI - Integral gain for generator PI torque controller [s]. (Only used in the transitional 2.5 region if VS_ControlMode =/ 2) +7.64 ! VS_TSRopt - Power-maximizing region 2 tip-speed-ratio. Only used in VS_ControlMode = 2. +0.314000000000 ! VS_PwrFiltF - Low pass filter on power used to determine generator speed set point. Only used in VS_ControlMode = 3. + +!------- SETPOINT SMOOTHER --------------------------------------------- +1.00000 ! SS_VSGain - Variable speed torque controller setpoint smoother gain, [-]. +0.00100 ! SS_PCGain - Collective pitch controller setpoint smoother gain, [-]. + +!------- POWER REFERENCE TRACKING -------------------------------------- +2 ! PRC_n - Number of elements in PRC_WindSpeeds and PRC_GenSpeeds array +0.07854 ! PRC_LPF_Freq - Frequency of the low pass filter on the wind speed estimate used to set PRC_GenSpeeds [rad/s] +3.0000 25.0000 ! PRC_WindSpeeds - Array of wind speeds used in rotor speed vs. wind speed lookup table [m/s] +0.7917 0.7917 ! PRC_GenSpeeds - Array of generator speeds corresponding to PRC_WindSpeeds [rad/s] + +!------- WIND SPEED ESTIMATOR --------------------------------------------- +63.000 ! WE_BladeRadius - Blade length (distance from hub center to blade tip), [m] +1 ! WE_CP_n - Amount of parameters in the Cp array +0.0 ! WE_CP - Parameters that define the parameterized CP(lambda) function +0.0 ! WE_Gamma - Adaption gain of the wind speed estimator algorithm [m/rad] +97.0 ! WE_GearboxRatio - Gearbox ratio [>=1], [-] +43702538.05700 ! WE_Jtot - Total drivetrain inertia, including blades, hub and casted generator inertia to LSS, [kg m^2] +1.225 ! WE_RhoAir - Air density, [kg m^-3] +"Cp_Ct_Cq.NREL5MW.txt" ! PerfFileName - File containing rotor performance tables (Cp,Ct,Cq) (absolute path or relative to this file) +36 26 ! PerfTableSize - Size of rotor performance tables, first number refers to number of blade pitch angles, second number referse to number of tip-speed ratios +60 ! WE_FOPoles_N - Number of first-order system poles used in EKF +3.0000 3.2897 3.5793 3.8690 4.1586 4.4483 4.7379 5.0276 5.3172 5.6069 5.8966 6.1862 6.4759 6.7655 7.0552 7.3448 7.6345 7.9241 8.2138 8.5034 8.7931 9.0828 9.3724 9.6621 9.9517 10.2414 10.5310 10.8207 11.1103 11.4000 11.8533 12.3067 12.7600 13.2133 13.6667 14.1200 14.5733 15.0267 15.4800 15.9333 16.3867 16.8400 17.2933 17.7467 18.2000 18.6533 19.1067 19.5600 20.0133 20.4667 20.9200 21.3733 21.8267 22.2800 22.7333 23.1867 23.6400 24.0933 24.5467 25.0000 ! WE_FOPoles_v - Wind speeds corresponding to first-order system poles [m/s] +-0.01640352 -0.01798730 -0.01957109 -0.02115488 -0.02273867 -0.02432245 -0.02590624 -0.02749003 -0.02907382 -0.03065761 -0.03224139 -0.03382518 -0.03540897 -0.03699276 -0.03857654 -0.04016033 -0.04174412 -0.04332791 -0.04491170 -0.04649548 -0.04807927 -0.04966306 -0.05124685 -0.05283063 -0.05441442 -0.05599821 -0.05763347 -0.05907205 -0.06912889 -0.05993737 -0.05021616 -0.05780794 -0.06849544 -0.08052122 -0.09351145 -0.10710432 -0.12106730 -0.13547025 -0.15041833 -0.16588021 -0.18135551 -0.19724989 -0.21342206 -0.22970423 -0.24663982 -0.26354532 -0.28064419 -0.29794214 -0.31532544 -0.33332004 -0.35128130 -0.36985759 -0.38827549 -0.40713466 -0.42584061 -0.44509747 -0.46449375 -0.48460700 -0.50475242 -0.52537402 ! WE_FOPoles - First order system poles [1/s] + +!------- YAW CONTROL ------------------------------------------------------ +0.00000 ! Y_uSwitch - Wind speed to switch between Y_ErrThresh. If zero, only the second value of Y_ErrThresh is used [m/s] +4.000000 8.000000 ! Y_ErrThresh - Yaw error threshold/deadbands. Turbine begins to yaw when it passes this. If Y_uSwitch is zero, only the second value is used. [deg]. +0.00870 ! Y_Rate - Yaw rate [rad/s] +0.00000 ! Y_MErrSet - Integrator saturation (maximum signal amplitude contribution to pitch from yaw-by-IPC), [rad] +0.00000 ! Y_IPC_IntSat - Integrator saturation (maximum signal amplitude contribution to pitch from yaw-by-IPC), [rad] +0.00000 ! Y_IPC_KP - Yaw-by-IPC proportional controller gain Kp +0.00000 ! Y_IPC_KI - Yaw-by-IPC integral controller gain Ki + +!------- TOWER CONTROL ------------------------------------------------------ +0.00000 ! TRA_ExclSpeed - Rotor speed for exclusion [LSS, rad/s] +0.00000 ! TRA_ExclBand - Size of the rotor frequency exclusion band [LSS, rad/s]. Torque controller reference will be TRA_ExclSpeed +/- TRA_ExlBand/2 +0.00000e+00 ! TRA_RateLimit - Rate limit of change in rotor speed reference [LSS, rad/s]. Suggested to be VS_RefSpd/400. +0.00000 ! FA_KI - Integral gain for the fore-aft tower damper controller, [rad*s/m] +0.00000 ! FA_HPFCornerFreq - Corner frequency (-3dB point) in the high-pass filter on the fore-aft acceleration signal [rad/s] +0.00000 ! FA_IntSat - Integrator saturation (maximum signal amplitude contribution to pitch from FA damper), [rad] + +!------- MINIMUM PITCH SATURATION ------------------------------------------- +60 ! PS_BldPitchMin_N - Number of values in minimum blade pitch lookup table (should equal number of values in PS_WindSpeeds and PS_BldPitchMin) +3.000 3.290 3.579 3.869 4.159 4.448 4.738 5.028 5.317 5.607 5.897 6.186 6.476 6.766 7.055 7.345 7.634 7.924 8.214 8.503 8.793 9.083 9.372 9.662 9.952 10.241 10.531 10.821 11.110 11.400 11.853 12.307 12.760 13.213 13.667 14.120 14.573 15.027 15.480 15.933 16.387 16.840 17.293 17.747 18.200 18.653 19.107 19.560 20.013 20.467 20.920 21.373 21.827 22.280 22.733 23.187 23.640 24.093 24.547 25.000 ! PS_WindSpeeds - Wind speeds corresponding to minimum blade pitch angles [m/s] +0.001 0.001 0.001 0.001 0.001 0.001 0.001 0.001 0.001 0.001 0.001 0.001 0.001 0.001 0.001 0.001 0.001 0.001 0.001 0.001 0.001 0.001 0.001 0.001 0.001 0.011 0.023 0.032 0.040 0.047 0.059 0.070 0.081 0.091 0.102 0.112 0.122 0.131 0.141 0.150 0.160 0.169 0.178 0.187 0.196 0.205 0.214 0.223 0.232 0.240 0.249 0.257 0.266 0.274 0.282 0.290 0.299 0.307 0.315 0.323 ! PS_BldPitchMin - Minimum blade pitch angles [rad] + +!------- SHUTDOWN ----------------------------------------------------------- +0.436300000000 ! SD_MaxPit - Maximum blade pitch angle to initiate shutdown, [rad] +0.418880000000 ! SD_CornerFreq - Cutoff Frequency for first order low-pass filter for blade pitch angle, [rad/s] + +!------- Floating ----------------------------------------------------------- +1 ! Fl_n - Number of Fl_Kp gains in gain scheduling, optional with default of 1 +0.0000 ! Fl_Kp - Nacelle velocity proportional feedback gain [s] +0.0000 ! Fl_U - Wind speeds for scheduling Fl_Kp, optional if Fl_Kp is single value [m/s] + +!------- FLAP ACTUATION ----------------------------------------------------- +0.000000000000 ! Flp_Angle - Initial or steady state flap angle [rad] +0.00000000e+00 ! Flp_Kp - Blade root bending moment proportional gain for flap control [s] +0.00000000e+00 ! Flp_Ki - Flap displacement integral gain for flap control [-] +0.174500000000 ! Flp_MaxPit - Maximum (and minimum) flap pitch angle [rad] + +!------- Open Loop Control ----------------------------------------------------- +"unused" ! OL_Filename - Input file with open loop timeseries (absolute path or relative to this file) +0 ! Ind_Breakpoint - The column in OL_Filename that contains the breakpoint (time if OL_Mode = 1) + 0 0 0 ! Ind_BldPitch - The columns in OL_Filename that contains the blade pitch (1,2,3) inputs in rad [array] +0 ! Ind_GenTq - The column in OL_Filename that contains the generator torque in Nm +0 ! Ind_YawRate - The column in OL_Filename that contains the yaw rate in rad/s +0 ! Ind_Azimuth - The column in OL_Filename that contains the desired azimuth position in rad (used if OL_Mode = 2) +0.0000 0.0000 0.0000 0.0000 ! RP_Gains - PID gains and Tf of derivative for rotor position control (used if OL_Mode = 2) +0 ! Ind_CableControl - The column(s) in OL_Filename that contains the cable control inputs in m [Used with CC_Mode = 2, must be the same size as CC_Group_N] +0 ! Ind_StructControl - The column(s) in OL_Filename that contains the structural control inputs [Used with StC_Mode = 2, must be the same size as StC_Group_N] + +!------- Pitch Actuator Model ----------------------------------------------------- +3.140000000000 ! PA_CornerFreq - Pitch actuator bandwidth/cut-off frequency [rad/s] +0.707000000000 ! PA_Damping - Pitch actuator damping ratio [-, unused if PA_Mode = 1] + +!------- Pitch Actuator Faults ----------------------------------------------------- +0.00000000 0.00000000 0.00000000 ! PF_Offsets - Constant blade pitch offsets for blades 1-3 [rad] + +!------- Active Wake Control ----------------------------------------------------- +1 ! AWC_NumModes - Number of user-defined AWC forcing modes +1 ! AWC_n - Azimuthal mode number(s) (i.e., the number and direction of the lobes of the wake structure) +1 ! AWC_harmonic - Harmonic(s) to apply in the AWC Inverse Coleman Transformation (only used when AWC_Mode = 2) +0.0500 ! AWC_freq - Frequency(s) of forcing mode(s) [Hz] +1.0000 ! AWC_amp - Pitch amplitude(s) of individual forcing mode(s) [deg] +0.0000 ! AWC_clockangle - Initial angle(s) of forcing mode(s) [deg] + +!------- External Controller Interface ----------------------------------------------------- +"unused" ! DLL_FileName - Name/location of the dynamic library in the Bladed-DLL format +"unused" ! DLL_InFile - Name of input file sent to the DLL (-) +"DISCON" ! DLL_ProcName - Name of procedure in DLL to be called (-) + +!------- ZeroMQ Interface --------------------------------------------------------- +"tcp://localhost:5556" ! ZMQ_CommAddress - Communication address for ZMQ server, (e.g. "tcp://localhost:5555") +1.000000 ! ZMQ_UpdatePeriod - Update period at zmq interface to send measurements and wait for setpoint [sec.] +2 ! ZMQ_ID - Integer identifier of turbine + +!------- Cable Control --------------------------------------------------------- +1 ! CC_Group_N - Number of cable control groups +0 ! CC_GroupIndex - First index for cable control group, should correspond to deltaL +20.000000 ! CC_ActTau - Time constant for line actuator [s] + +!------- Structural Controllers --------------------------------------------------------- +1 ! StC_Group_N - Number of cable control groups +0 ! StC_GroupIndex - First index for structural control group, options specified in ServoDyn summary output diff --git a/examples/FAST.Farm_interface/inputs/FFFiles/FFarm_mod.fstf b/examples/FAST.Farm_interface/inputs/FFFiles/FFarm_mod.fstf new file mode 100644 index 00000000..d831c0f5 --- /dev/null +++ b/examples/FAST.Farm_interface/inputs/FFFiles/FFarm_mod.fstf @@ -0,0 +1,106 @@ +------- FAST.Farm for OpenFAST INPUT FILE ------------------------------------------------- +FAST.Farm input - file, using two turbines separated by 3D downstream and an offset of 30m, with a turbulent inflow given by one turbsim box +--- SIMULATION CONTROL --- +False Echo - Echo input data to .ech? (flag) +FATAL AbortLevel - Error level when simulation should abort (string) {"WARNING", "SEVERE", "FATAL"} +60 TMax - Total run time (s) [>=0.0] +2 Mod_AmbWind - Ambient wind model (-) (switch) {1: high-fidelity precursor in VTK format, 2: InflowWind module} +2 Mod_WaveField - Wave field handling (-) (switch) {1: use individual HydroDyn inputs without adjustment, 2: adjust wave phases based on turbine offsets from farm origin} +0 Mod_SharedMooring - Shared mooring system model (switch) {0: None, 3=MoorDyn}} +--- SHARED MOORING SYSTEM --- [used only for Mod_SharedMoor>0] +"" SharedMoorFile - Name of file containing shared mooring system input parameters (quoted string) [used only when Mod_SharedMooring > 0] +0.04 DT_Mooring - Time step for farm-level mooring coupling with each turbine (s) [used only when Mod_SharedMooring > 0] +true WrMooringVis - Write shared mooring visualization, at the global FAST.Farm time step (-) [only used for Mod_SharedMooring=3] +--- AMBIENT WIND: PRECURSOR IN VTK FORMAT --- [used only for Mod_AmbWind=1] +2.0 DT_Low-VTK - Time step for low -resolution wind data input files; will be used as the global FAST.Farm time step (s) [>0.0] +0.1 DT_High-VTK - Time step for high-resolution wind data input files (s) [>0.0] +"unused" WindFilePath - Path name to wind data files from precursor (string) +False ChkWndFiles - Check all the ambient wind files for data consistency? (flag) +--- AMBIENT WIND: INFLOWWIND MODULE --- [used only for Mod_AmbWind=2 or 3] +3.0 DT_Low - Time step for low -resolution wind data interpolation; will be used as the global FAST.Farm time step (s) [>0.0] +0.25 DT_High - Time step for high-resolution wind data interpolation (s) [>0.0] +100 NX_Low - Number of low -resolution spatial nodes in X direction for wind data interpolation (-) [>=2] +83 NY_Low - Number of low -resolution spatial nodes in Y direction for wind data interpolation (-) [>=2] +39 NZ_Low - Number of low -resolution spatial nodes in Z direction for wind data interpolation (-) [>=2] +-360 X0_Low - Origin of low -resolution spatial nodes in X direction for wind data interpolation (m) +-382.0 Y0_Low - Origin of low -resolution spatial nodes in Y direction for wind data interpolation (m) +1.0 Z0_Low - Origin of low -resolution spatial nodes in Z direction for wind data interpolation (m) +24 dX_Low - Spacing of low -resolution spatial nodes in X direction for wind data interpolation (m) [>0.0] +9.3 dY_Low - Spacing of low -resolution spatial nodes in Y direction for wind data interpolation (m) [>0.0] +9.3 dZ_Low - Spacing of low -resolution spatial nodes in Z direction for wind data interpolation (m) [>0.0] +39 NX_High - Number of high-resolution spatial nodes in X direction for wind data interpolation (-) [>=2] +35 NY_High - Number of high-resolution spatial nodes in Y direction for wind data interpolation (-) [>=2] +37 NZ_High - Number of high-resolution spatial nodes in Z direction for wind data interpolation (-) [>=2] +"./NRELOffshrBsline5MW_InflowWind_Steady8mps.dat" InflowFile - Name of file containing InflowWind module input parameters (quoted string) +--- WIND TURBINES --- +3 NumTurbines - Number of wind turbines (-) [>=1] [last 6 columns used only for Mod_AmbWind=2] +WT_X WT_Y WT_Z WT_FASTInFile X0_High Y0_High Z0_High dX_High dY_High dZ_High +(m) (m) (m) (string) (m) (m) (m) (m) (m) (m) +0 0 0 "5MW_Land_DLL_WTurb.T1.fst" -76 -7.97500000e+01 1 4 4.65000000e+00 4.65000000e+00 +504 0 0 "5MW_Land_DLL_WTurb.T2.fst" 428 -7.97500000e+01 1 4 4.65000000e+00 4.65000000e+00 +1008 0 0 "5MW_Land_DLL_WTurb.T3.fst" 932 -7.97500000e+01 1 4 4.65000000e+00 4.65000000e+00 +--- WAKE DYNAMICS --- +1 Mod_Wake - Switch between wake formulations {1:Polar, 2:Curl, 3:Cartesian} (-) (switch) +125 RotorDiamRef - Reference turbine rotor diameter for wake calculations (m) [>0.0] +4.65 dr - Radial increment of radial finite-difference grid (m) [>0.0] +42 NumRadii - Number of radii in the radial finite-difference grid (-) [>=2] +126 NumPlanes - Number of wake planes (-) [>=2] +DEFAULT f_c - Cutoff (corner) frequency of the low-pass time-filter for the wake advection, deflection, and meandering model (Hz) [>0.0] or DEFAULT [DEFAULT=0.0007] +DEFAULT C_HWkDfl_O - Calibrated parameter in the correction for wake deflection defining the horizontal offset at the rotor (m ) or DEFAULT [DEFAULT= 0.0 ] +DEFAULT C_HWkDfl_OY - Calibrated parameter in the correction for wake deflection defining the horizontal offset at the rotor scaled with yaw error (m/deg) or DEFAULT [DEFAULT= 0.3 ] +DEFAULT C_HWkDfl_x - Calibrated parameter in the correction for wake deflection defining the horizontal offset scaled with downstream distance (- ) or DEFAULT [DEFAULT= 0.0 ] +DEFAULT C_HWkDfl_xY - Calibrated parameter in the correction for wake deflection defining the horizontal offset scaled with downstream distance and yaw error (1/deg) or DEFAULT [DEFAULT=-0.004] +DEFAULT C_NearWake - Calibrated parameter for the near-wake correction (-) [>1.0 and <2.5] or DEFAULT [DEFAULT=1.8] +DEFAULT k_vAmb - Calibrated parameter for the influence of ambient turbulence in the eddy viscosity (-) [>=0.0] or DEFAULT [DEFAULT=0.05 ] +DEFAULT k_vShr - Calibrated parameter for the influence of the shear layer in the eddy viscosity (-) [>=0.0] or DEFAULT [DEFAULT=0.016] +DEFAULT Mod_WakeDiam - Wake diameter calculation model (-) (switch) {1: rotor diameter, 2: velocity based, 3: mass-flux based, 4: momentum-flux based} or DEFAULT [DEFAULT=1] +DEFAULT C_WakeDiam - Calibrated parameter for wake diameter calculation (-) [>0.0 and <0.99] or DEFAULT [DEFAULT=0.95] [unused for Mod_WakeDiam=1] +DEFAULT Mod_Meander - Spatial filter model for wake meandering (-) (switch) {1: uniform, 2: truncated jinc, 3: windowed jinc} or DEFAULT [DEFAULT=3] +DEFAULT C_Meander - Calibrated parameter for wake meandering (-) [>=1.0] or DEFAULT [DEFAULT=1.9] +--- CURLED-WAKE PARAMETERS [only used if Mod_Wake=2 or 3] --- +DEFAULT Swirl - Switch to include swirl velocities in wake (-) (switch) [DEFAULT=TRUE] +DEFAULT k_VortexDecay - Vortex decay constant for curl (-) [DEFAULT=0] +DEFAULT NumVortices - The number of vortices in the curled wake model (-) [DEFAULT=100] +DEFAULT sigma_D - The width of the vortices in the curled wake model non-dimesionalized by rotor diameter (-) [DEFAULT=0.2] +DEFAULT FilterInit - Switch to filter the initial wake plane deficit and select the number of grid points for the filter {0: no filter, 1: filter of size 1} or DEFAULT [DEFAULT=1] (switch) +DEFAULT k_vCurl - Calibrated parameter for scaling the eddy viscosity in the curled-wake model (-) [>=0] or DEFAULT [DEFAULT=2.0 ] +DEFAULT Mod_Projection - Switch to select how the wake plane velocity is projected in AWAE {1: keep all components, 2: project against plane normal} or DEFAULT [DEFAULT=1: if Mod_Wake is 1 or 3, or DEFAULT=2: if Mod_Wake is 2] (switch) +--- WAKE-ADDED TURBULENCE --- +0 WAT - Switch between wake-added turbulence box options {0: no wake added turbulence, 1: predefined turbulence box, 2: user defined turbulence box} (switch) +"../WAT_MannBoxDB/FFDB_D100_512x512x64.u" WAT_BoxFile - Filepath to the file containing the u-component of the turbulence box (either predefined or user-defined) (quoted string) +512, 512, 64 WAT_NxNyNz - Number of points in the x, y, and z directions of the WAT_BoxFile [used only if WAT=2, derived value if WAT=1] (-) +5.0, 5.0, 5.0 WAT_DxDyDz - Distance (in meters) between points in the x, y, and z directions of the WAT_BoxFile [used only if WAT=2, derived value if WAT=1] (m) +default WAT_ScaleBox - Flag to scale the input turbulence box to zero mean and unit standard deviation at every node [DEFAULT=False] (flag) +default WAT_k_Def - Calibrated parameters for the influence of the maximum wake deficit on wake-added turbulence (set of 5 parameters: k_Def, FMin, DMin, DMax, Exp) (-) [>=0.0, >=0.0 and <=1.0, >=0.0, >DMin, >=0.0] or DEFAULT [DEFAULT=[0.6, 0.0, 0.0, 2.0, 1.0 ]] +default WAT_k_Grad - Calibrated parameters for the influence of the radial velocity gradient of the wake deficit on wake-added turbulence (set of 5 parameters: k_Grad, FMin, DMin, DMax, Exp) (-) [>=0.0, >=0.0 and <=1.0, >=0.0, >DMin, >=0.0] or DEFAULT [DEFAULT=[3.0, 0.0, 0.0, 12.0, 0.65] +--- VISUALIZATION --- +False WrDisWind - Write low- and high-resolution disturbed wind data to .Low.Dis.t.vtk etc.? (flag) +0 NOutDisWindXY - Number of XY planes for output of disturbed wind data across the low-resolution domain to .Low.DisXY.t.vtk (-) [0 to 9] +80.0 OutDisWindZ - Z coordinates of XY planes for output of disturbed wind data across the low-resolution domain (m) [1 to NOutDisWindXY] [unused for NOutDisWindXY=0] +0 NOutDisWindYZ - Number of YZ planes for output of disturbed wind data across the low-resolution domain to /Low.DisYZ.t.vtk (-) [0 to 9] +748.0, 1252.0, 1378.0, 1504.0, 1630.0, 1756.0, 1882.0, 2008.0 OutDisWindX - X coordinates of YZ planes for output of disturbed wind data across the low-resolution domain (m) [1 to NOutDisWindYZ] [unused for NOutDisWindYZ=0] +0 NOutDisWindXZ - Number of XZ planes for output of disturbed wind data across the low-resolution domain to /Low.DisXZ.t.vtk (-) [0 to 9] +0.0 OutDisWindY - Y coordinates of XZ planes for output of disturbed wind data across the low-resolution domain (m) [1 to NOutDisWindXZ] [unused for NOutDisWindXZ=0] +DEFAULT WrDisDT - Time step for disturbed wind visualization output (s) [>0.0] or DEFAULT [DEFAULT=DT_Low or DT_Low-VTK] [unused for WrDisWind=False and NOutDisWindXY=NOutDisWindYZ=NOutDisWindXZ=0] +--- OUTPUT --- +False SumPrint - Print summary data to .sum? (flag) +99999.9 ChkptTime - Amount of time between creating checkpoint files for potential restart (s) [>0.0] +0.0 TStart - Time to begin tabular output (s) [>=0.0] +1 OutFileFmt - Format for tabular (time-marching) output file (switch) {1: text file [.out], 2: binary file [.outb], 3: both} +True TabDelim - Use tab delimiters in text tabular output file? (flag) {uses spaces if False} +"ES10.3E2" OutFmt - Format used for text tabular output, excluding the time channel. Resulting field should be 10 characters. (quoted string) +DEFAULT OutAllPlanes - Output all wake planes at all time steps. [DEFAULT=False] +0 NOutRadii - Number of radial nodes for wake output for an individual rotor (-) [0 to 20] +0, 1, 2, 3, 4, 5, 7, 9, 11, 13, 15, 16, 17, 18, 19, 21, 24, 28, 33, 39 OutRadii - List of radial nodes for wake output for an individual rotor (-) [1 to NOutRadii] [unused for NOutRadii=0] +0 NOutDist - Number of downstream distances for wake output for an individual rotor (-) [0 to 9 ] +252.0, 378.0, 504.0, 630.0, 756.0, 882.0, 1008.0 OutDist - List of downstream distances for wake output for an individual rotor (m) [1 to NOutDist ] [unused for NOutDist =0] +0 NWindVel - Number of points for wind output (-) [0 to 9] +0.0 WindVelX - List of coordinates in the X direction for wind output (m) [1 to NWindVel] [unused for NWindVel=0] +0.0 WindVelY - List of coordinates in the Y direction for wind output (m) [1 to NWindVel] [unused for NWindVel=0] +80.0 WindVelZ - List of coordinates in the Z direction for wind output (m) [1 to NWindVel] [unused for NWindVel=0] + OutList The next line(s) contains a list of output parameters. See OutListParameters.xlsx for a listing of available output channels (quoted string) +"RtAxsXT1" +"RtAxsXT2" +"RtAxsXT3" +END +--------------------------------------------------------------------------------------- \ No newline at end of file diff --git a/examples/FAST.Farm_interface/inputs/FFFiles/NRELOffshrBsline5MW_AeroDyn_blade.dat b/examples/FAST.Farm_interface/inputs/FFFiles/NRELOffshrBsline5MW_AeroDyn_blade.dat new file mode 100644 index 00000000..c20a62e7 --- /dev/null +++ b/examples/FAST.Farm_interface/inputs/FFFiles/NRELOffshrBsline5MW_AeroDyn_blade.dat @@ -0,0 +1,28 @@ +------- AERODYN v15.00.* BLADE DEFINITION INPUT FILE ------------------------------------- +NREL 5.0 MW offshore baseline aerodynamic blade input properties; note that we need to add the aerodynamic center to this file +====== Blade Properties ================================================================= + 19 NumBlNds - Number of blade nodes used in the analysis (-) + BlSpn BlCrvAC BlSwpAC BlCrvAng BlTwist BlChord BlAFID BlCb BlCenBn BlCenBt + (m) (m) (m) (deg) (deg) (m) (-) (-) (m) (m) +0.0000000E+00 0.0000000E+00 0.0000000E+00 0.0000000E+00 1.3308000E+01 3.5420000E+00 1 0.0 0.0 0.0 +1.3667000E+00 -8.1531745E-04 -3.4468858E-03 0.0000000E+00 1.3308000E+01 3.5420000E+00 1 0.0 0.0 0.0 +4.1000000E+00 -2.4839790E-02 -1.0501421E-01 0.0000000E+00 1.3308000E+01 3.8540000E+00 1 0.0 0.0 0.0 +6.8333000E+00 -5.9469375E-02 -2.5141635E-01 0.0000000E+00 1.3308000E+01 4.1670000E+00 2 0.0 0.0 0.0 +1.0250000E+01 -1.0909141E-01 -4.6120149E-01 0.0000000E+00 1.3308000E+01 4.5570000E+00 3 0.0 0.0 0.0 +1.4350000E+01 -1.1573354E-01 -5.6986665E-01 0.0000000E+00 1.1480000E+01 4.6520000E+00 4 0.0 0.0 0.0 +1.8450000E+01 -9.8316709E-02 -5.4850833E-01 0.0000000E+00 1.0162000E+01 4.4580000E+00 4 0.0 0.0 0.0 +2.2550000E+01 -8.3186967E-02 -5.2457001E-01 0.0000000E+00 9.0110000E+00 4.2490000E+00 5 0.0 0.0 0.0 +2.6650000E+01 -6.7933232E-02 -4.9624675E-01 0.0000000E+00 7.7950000E+00 4.0070000E+00 6 0.0 0.0 0.0 +3.0750000E+01 -5.3393159E-02 -4.6544755E-01 0.0000000E+00 6.5440000E+00 3.7480000E+00 6 0.0 0.0 0.0 +3.4850000E+01 -4.0899260E-02 -4.3583519E-01 0.0000000E+00 5.3610000E+00 3.5020000E+00 7 0.0 0.0 0.0 +3.8950000E+01 -2.9722933E-02 -4.0591323E-01 0.0000000E+00 4.1880000E+00 3.2560000E+00 7 0.0 0.0 0.0 +4.3050000E+01 -2.0511081E-02 -3.7569051E-01 0.0000000E+00 3.1250000E+00 3.0100000E+00 8 0.0 0.0 0.0 +4.7150000E+01 -1.3980013E-02 -3.4521705E-01 0.0000000E+00 2.3190000E+00 2.7640000E+00 8 0.0 0.0 0.0 +5.1250000E+01 -8.3819737E-03 -3.1463837E-01 0.0000000E+00 1.5260000E+00 2.5180000E+00 8 0.0 0.0 0.0 +5.4666700E+01 -4.3546914E-03 -2.8909220E-01 0.0000000E+00 8.6300000E-01 2.3130000E+00 8 0.0 0.0 0.0 +5.7400000E+01 -1.6838383E-03 -2.6074456E-01 0.0000000E+00 3.7000000E-01 2.0860000E+00 8 0.0 0.0 0.0 +6.0133300E+01 -3.2815226E-04 -1.7737470E-01 0.0000000E+00 1.0600000E-01 1.4190000E+00 8 0.0 0.0 0.0 +6.1499900E+01 -3.2815226E-04 -1.7737470E-01 0.0000000E+00 1.0600000E-01 1.4190000E+00 8 0.0 0.0 0.0 + +!bjj: because of precision in the BD-AD coupling, 61.5m didn't work, so I changed it to 61.4999m +6.1500000E+01 -3.2815226E-04 -1.7737470E-01 0.0000000E+00 1.0600000E-01 1.4190000E+00 8 0.0 0.0 0.0 diff --git a/examples/FAST.Farm_interface/inputs/FFFiles/NRELOffshrBsline5MW_Blade.dat b/examples/FAST.Farm_interface/inputs/FFFiles/NRELOffshrBsline5MW_Blade.dat new file mode 100644 index 00000000..4ceba92c --- /dev/null +++ b/examples/FAST.Farm_interface/inputs/FFFiles/NRELOffshrBsline5MW_Blade.dat @@ -0,0 +1,83 @@ +------- ELASTODYN V1.00.* INDIVIDUAL BLADE INPUT FILE -------------------------- +NREL 5.0 MW offshore baseline blade input properties. +---------------------- BLADE PARAMETERS ---------------------------------------- + 49 NBlInpSt - Number of blade input stations (-) + 0.477465 BldFlDmp(1) - Blade flap mode #1 structural damping in percent of critical (%) + 0.477465 BldFlDmp(2) - Blade flap mode #2 structural damping in percent of critical (%) + 0.477465 BldEdDmp(1) - Blade edge mode #1 structural damping in percent of critical (%) +---------------------- BLADE ADJUSTMENT FACTORS -------------------------------- + 1 FlStTunr(1) - Blade flapwise modal stiffness tuner, 1st mode (-) + 1 FlStTunr(2) - Blade flapwise modal stiffness tuner, 2nd mode (-) + 1.04536 AdjBlMs - Factor to adjust blade mass density (-) !bjj: value for AD14=1.04536; value for AD15=1.057344 (it would be nice to enter the requested blade mass instead of a factor here) + 1 AdjFlSt - Factor to adjust blade flap stiffness (-) + 1 AdjEdSt - Factor to adjust blade edge stiffness (-) +---------------------- DISTRIBUTED BLADE PROPERTIES ---------------------------- + BlFract PitchAxis StrcTwst BMassDen FlpStff EdgStff + (-) (-) (deg) (kg/m) (Nm^2) (Nm^2) +0.0000000E+00 2.5000000E-01 1.3308000E+01 6.7893500E+02 1.8110000E+10 1.8113600E+10 +3.2500000E-03 2.5000000E-01 1.3308000E+01 6.7893500E+02 1.8110000E+10 1.8113600E+10 +1.9510000E-02 2.5049000E-01 1.3308000E+01 7.7336300E+02 1.9424900E+10 1.9558600E+10 +3.5770000E-02 2.5490000E-01 1.3308000E+01 7.4055000E+02 1.7455900E+10 1.9497800E+10 +5.2030000E-02 2.6716000E-01 1.3308000E+01 7.4004200E+02 1.5287400E+10 1.9788800E+10 +6.8290000E-02 2.7941000E-01 1.3308000E+01 5.9249600E+02 1.0782400E+10 1.4858500E+10 +8.4550000E-02 2.9167000E-01 1.3308000E+01 4.5027500E+02 7.2297200E+09 1.0220600E+10 +1.0081000E-01 3.0392000E-01 1.3308000E+01 4.2405400E+02 6.3095400E+09 9.1447000E+09 +1.1707000E-01 3.1618000E-01 1.3308000E+01 4.0063800E+02 5.5283600E+09 8.0631600E+09 +1.3335000E-01 3.2844000E-01 1.3308000E+01 3.8206200E+02 4.9800600E+09 6.8844400E+09 +1.4959000E-01 3.4069000E-01 1.3308000E+01 3.9965500E+02 4.9368400E+09 7.0091800E+09 +1.6585000E-01 3.5294000E-01 1.3308000E+01 4.2632100E+02 4.6916600E+09 7.1676800E+09 +1.8211000E-01 3.6519000E-01 1.3181000E+01 4.1682000E+02 3.9494600E+09 7.2716600E+09 +1.9837000E-01 3.7500000E-01 1.2848000E+01 4.0618600E+02 3.3865200E+09 7.0817000E+09 +2.1465000E-01 3.7500000E-01 1.2192000E+01 3.8142000E+02 2.9337400E+09 6.2445300E+09 +2.3089000E-01 3.7500000E-01 1.1561000E+01 3.5282200E+02 2.5689600E+09 5.0489600E+09 +2.4715000E-01 3.7500000E-01 1.1072000E+01 3.4947700E+02 2.3886500E+09 4.9484900E+09 +2.6341000E-01 3.7500000E-01 1.0792000E+01 3.4653800E+02 2.2719900E+09 4.8080200E+09 +2.9595000E-01 3.7500000E-01 1.0232000E+01 3.3933300E+02 2.0500500E+09 4.5014000E+09 +3.2846000E-01 3.7500000E-01 9.6720000E+00 3.3000400E+02 1.8282500E+09 4.2440700E+09 +3.6098000E-01 3.7500000E-01 9.1100000E+00 3.2199000E+02 1.5887100E+09 3.9952800E+09 +3.9350000E-01 3.7500000E-01 8.5340000E+00 3.1382000E+02 1.3619300E+09 3.7507600E+09 +4.2602000E-01 3.7500000E-01 7.9320000E+00 2.9473400E+02 1.1023800E+09 3.4471400E+09 +4.5855000E-01 3.7500000E-01 7.3210000E+00 2.8712000E+02 8.7580000E+08 3.1390700E+09 +4.9106000E-01 3.7500000E-01 6.7110000E+00 2.6334300E+02 6.8130000E+08 2.7342400E+09 +5.2358000E-01 3.7500000E-01 6.1220000E+00 2.5320700E+02 5.3472000E+08 2.5548700E+09 +5.5610000E-01 3.7500000E-01 5.5460000E+00 2.4166600E+02 4.0890000E+08 2.3340300E+09 +5.8862000E-01 3.7500000E-01 4.9710000E+00 2.2063800E+02 3.1454000E+08 1.8287300E+09 +6.2115000E-01 3.7500000E-01 4.4010000E+00 2.0029300E+02 2.3863000E+08 1.5841000E+09 +6.5366000E-01 3.7500000E-01 3.8340000E+00 1.7940400E+02 1.7588000E+08 1.3233600E+09 +6.8618000E-01 3.7500000E-01 3.3320000E+00 1.6509400E+02 1.2601000E+08 1.1836800E+09 +7.1870000E-01 3.7500000E-01 2.8900000E+00 1.5441100E+02 1.0726000E+08 1.0201600E+09 +7.5122000E-01 3.7500000E-01 2.5030000E+00 1.3893500E+02 9.0880000E+07 7.9781000E+08 +7.8376000E-01 3.7500000E-01 2.1160000E+00 1.2955500E+02 7.6310000E+07 7.0961000E+08 +8.1626000E-01 3.7500000E-01 1.7300000E+00 1.0726400E+02 6.1050000E+07 5.1819000E+08 +8.4878000E-01 3.7500000E-01 1.3420000E+00 9.8776000E+01 4.9480000E+07 4.5487000E+08 +8.8130000E-01 3.7500000E-01 9.5400000E-01 9.0248000E+01 3.9360000E+07 3.9512000E+08 +8.9756000E-01 3.7500000E-01 7.6000000E-01 8.3001000E+01 3.4670000E+07 3.5372000E+08 +9.1382000E-01 3.7500000E-01 5.7400000E-01 7.2906000E+01 3.0410000E+07 3.0473000E+08 +9.3008000E-01 3.7500000E-01 4.0400000E-01 6.8772000E+01 2.6520000E+07 2.8142000E+08 +9.3821000E-01 3.7500000E-01 3.1900000E-01 6.6264000E+01 2.3840000E+07 2.6171000E+08 +9.4636000E-01 3.7500000E-01 2.5300000E-01 5.9340000E+01 1.9630000E+07 1.5881000E+08 +9.5447000E-01 3.7500000E-01 2.1600000E-01 5.5914000E+01 1.6000000E+07 1.3788000E+08 +9.6260000E-01 3.7500000E-01 1.7800000E-01 5.2484000E+01 1.2830000E+07 1.1879000E+08 +9.7073000E-01 3.7500000E-01 1.4000000E-01 4.9114000E+01 1.0080000E+07 1.0163000E+08 +9.7886000E-01 3.7500000E-01 1.0100000E-01 4.5818000E+01 7.5500000E+06 8.5070000E+07 +9.8699000E-01 3.7500000E-01 6.2000000E-02 4.1669000E+01 4.6000000E+06 6.4260000E+07 +9.9512000E-01 3.7500000E-01 2.3000000E-02 1.1453000E+01 2.5000000E+05 6.6100000E+06 +1.0000000E+00 3.7500000E-01 0.0000000E+00 1.0319000E+01 1.7000000E+05 5.0100000E+06 +---------------------- BLADE MODE SHAPES --------------------------------------- + 0.0622 BldFl1Sh(2) - Flap mode 1, coeff of x^2 + 1.7254 BldFl1Sh(3) - , coeff of x^3 + -3.2452 BldFl1Sh(4) - , coeff of x^4 + 4.7131 BldFl1Sh(5) - , coeff of x^5 + -2.2555 BldFl1Sh(6) - , coeff of x^6 + -0.5809 BldFl2Sh(2) - Flap mode 2, coeff of x^2 + 1.2067 BldFl2Sh(3) - , coeff of x^3 + -15.5349 BldFl2Sh(4) - , coeff of x^4 + 29.7347 BldFl2Sh(5) - , coeff of x^5 + -13.8255 BldFl2Sh(6) - , coeff of x^6 + 0.3627 BldEdgSh(2) - Edge mode 1, coeff of x^2 + 2.5337 BldEdgSh(3) - , coeff of x^3 + -3.5772 BldEdgSh(4) - , coeff of x^4 + 2.376 BldEdgSh(5) - , coeff of x^5 + -0.6952 BldEdgSh(6) - , coeff of x^6 + + diff --git a/examples/FAST.Farm_interface/inputs/FFFiles/NRELOffshrBsline5MW_InflowWind_Steady8mps.dat b/examples/FAST.Farm_interface/inputs/FFFiles/NRELOffshrBsline5MW_InflowWind_Steady8mps.dat new file mode 100644 index 00000000..8be0c8e7 --- /dev/null +++ b/examples/FAST.Farm_interface/inputs/FFFiles/NRELOffshrBsline5MW_InflowWind_Steady8mps.dat @@ -0,0 +1,71 @@ +------- InflowWind INPUT FILE ------------------------------------------------------------------------- +Steady m/s - winds with no shear for FAST CertTests #20 and #25 +--------------------------------------------------------------------------------------------------------------- +False Echo - Echo input data to .ech (flag) +3 WindType - switch for wind file type (1=steady; 2=uniform; 3=binary TurbSim FF; 4=binary Bladed-style FF; 5=HAWC format; 6=User defined; 7=native Bladed FF) +0 PropagationDir - Direction of wind propagation (meteorological rotation from aligned with X (positive rotates towards -Y) -- degrees) (not used for native Bladed format WindType=7) +0 VFlowAng - Upflow angle (degrees) (not used for native Bladed format WindType=7) +False VelInterpCubic - Use cubic interpolation for velocity in time (false=linear, true=cubic) [Used with WindType=2,3,4,5,7] +1 NWindVel - Number of points to output the wind velocity (0 to 9) +0 WindVxiList - List of coordinates in the inertial X direction (m) +0 WindVyiList - List of coordinates in the inertial Y direction (m) +90 WindVziList - List of coordinates in the inertial Z direction (m) +================== Parameters for Steady Wind Conditions [used only for WindType = 1] ========================= +8 HWindSpeed - Horizontal wind speed (m/s) +90 RefHt - Reference height for horizontal wind speed (m) +0 PLExp - Power law exponent (-) +================== Parameters for Uniform wind file [used only for WindType = 2] ============================ +"unused" Filename_Uni - Filename of time series data for uniform wind field. (-) +90 RefHt_Uni - Reference height for horizontal wind speed (m) +125.88 RefLength - Reference length for linear horizontal and vertical sheer (-) +================== Parameters for Binary TurbSim Full-Field files [used only for WindType = 3] ============== +"./TurbSim/Low.bts" FileName_BTS - Name of the Full field wind file to use (.bts) +================== Parameters for Binary Bladed-style Full-Field files [used only for WindType = 4 or WindType = 7] ========= +"unused" FileNameRoot - WindType=4: Rootname of the full-field wind file to use (.wnd, .sum); WindType=7: name of the intermediate file with wind scaling values +False TowerFile - Have tower file (.twr) (flag) ignored when WindType = 7 +================== Parameters for HAWC-format binary files [Only used with WindType = 5] ===================== +"wasp\Output\basic_5u.bin" FileName_u - name of the file containing the u-component fluctuating wind (.bin) +"wasp\Output\basic_5v.bin" FileName_v - name of the file containing the v-component fluctuating wind (.bin) +"wasp\Output\basic_5w.bin" FileName_w - name of the file containing the w-component fluctuating wind (.bin) +64 nx - number of grids in the x direction (in the 3 files above) (-) +32 ny - number of grids in the y direction (in the 3 files above) (-) +32 nz - number of grids in the z direction (in the 3 files above) (-) +16 dx - distance (in meters) between points in the x direction (m) +3 dy - distance (in meters) between points in the y direction (m) +3 dz - distance (in meters) between points in the z direction (m) +90 RefHt_Hawc - reference height; the height (in meters) of the vertical center of the grid (m) + ------------- Scaling parameters for turbulence --------------------------------------------------------- +1 ScaleMethod - Turbulence scaling method [0 = none, 1 = direct scaling, 2 = calculate scaling factor based on a desired standard deviation] +1 SFx - Turbulence scaling factor for the x direction (-) [ScaleMethod=1] +1 SFy - Turbulence scaling factor for the y direction (-) [ScaleMethod=1] +1 SFz - Turbulence scaling factor for the z direction (-) [ScaleMethod=1] +12 SigmaFx - Turbulence standard deviation to calculate scaling from in x direction (m/s) [ScaleMethod=2] +8 SigmaFy - Turbulence standard deviation to calculate scaling from in y direction (m/s) [ScaleMethod=2] +2 SigmaFz - Turbulence standard deviation to calculate scaling from in z direction (m/s) [ScaleMethod=2] + ------------- Mean wind profile parameters (added to HAWC-format files) --------------------------------- +5 URef - Mean u-component wind speed at the reference height (m/s) +2 WindProfile - Wind profile type (0=constant;1=logarithmic,2=power law) +0 PLExp_Hawc - Power law exponent (-) (used for PL wind profile type only) +0.03 Z0 - Surface roughness length (m) (used for LG wind profile type only) +0 XOffset - Initial offset in +x direction (shift of wind box) +================== LIDAR Parameters =========================================================================== +0 SensorType - Switch for lidar configuration (0 = None, 1 = Single Point Beam(s), 2 = Continuous, 3 = Pulsed) +0 NumPulseGate - Number of lidar measurement gates (used when SensorType = 3) +30 PulseSpacing - Distance between range gates (m) (used when SensorType = 3) +0 NumBeam - Number of lidar measurement beams (0-5)(used when SensorType = 1) +-200 FocalDistanceX - Focal distance co-ordinates of the lidar beam in the x direction (relative to hub height) (only first coordinate used for SensorType 2 and 3) (m) +0 FocalDistanceY - Focal distance co-ordinates of the lidar beam in the y direction (relative to hub height) (only first coordinate used for SensorType 2 and 3) (m) +0 FocalDistanceZ - Focal distance co-ordinates of the lidar beam in the z direction (relative to hub height) (only first coordinate used for SensorType 2 and 3) (m) +0.0, 0.0, 0.0 RotorApexOffsetPos - Offset of the lidar from hub height (m) +17 URefLid - Reference average wind speed for the lidar[m/s] +0.25 MeasurementInterval - Time between each measurement [s] +False LidRadialVel - TRUE => return radial component, FALSE => return 'x' direction estimate +1 ConsiderHubMotion - Flag whether to consider the hub motion's impact on Lidar measurements +====================== OUTPUT ================================================== +False SumPrint - Print summary data to .IfW.sum (flag) + OutList The next line(s) contains a list of output parameters. See OutListParameters.xlsx for a listing of available output channels, (-) +"Wind1VelX" X-direction wind velocity at point WindList(1) +"Wind1VelY" Y-direction wind velocity at point WindList(1) +"Wind1VelZ" Z-direction wind velocity at point WindList(1) +END +--------------------------------------------------------------------------------------- \ No newline at end of file diff --git a/examples/FAST.Farm_interface/inputs/FFFiles/NRELOffshrBsline5MW_Onshore_AeroDyn15.dat b/examples/FAST.Farm_interface/inputs/FFFiles/NRELOffshrBsline5MW_Onshore_AeroDyn15.dat new file mode 100644 index 00000000..f1e542ec --- /dev/null +++ b/examples/FAST.Farm_interface/inputs/FFFiles/NRELOffshrBsline5MW_Onshore_AeroDyn15.dat @@ -0,0 +1,117 @@ +------- AERODYN v15 for OpenFAST INPUT FILE ----------------------------------------------- +NREL 5.0 MW offshore baseline aerodynamic input properties. +====== General Options ============================================================================ +False Echo - Echo the input to ".AD.ech"? (flag) +"default" DTAero - Time interval for aerodynamic calculations {or "default"} (s) +1 Wake_Mod - Wake/induction model (switch) {0=none, 1=BEMT, 3=OLAF} [Wake_Mod cannot be 2 or 3 when linearizing] +0 TwrPotent - Type tower influence on wind based on potential flow around the tower (switch) {0=none, 1=baseline potential flow, 2=potential flow with Bak correction} +0 TwrShadow - Calculate tower influence on wind based on downstream tower shadow (switch) {0=none, 1=Powles model, 2=Eames model} +False TwrAero - Calculate tower aerodynamic loads? (flag) +False CavitCheck - Perform cavitation check? (flag) [UA_Mod must be 0 when CavitCheck=true] +False Buoyancy - Include buoyancy effects? (flag) +False NacelleDrag - Include Nacelle Drag effects? (flag) +False CompAA - Flag to compute AeroAcoustics calculation [used only when Wake_Mod = 1 or 2] +"unused" AA_InputFile - AeroAcoustics input file [used only when CompAA=true] +====== Environmental Conditions =================================================================== +"default" AirDens - Air density (kg/m^3) +"default" KinVisc - Kinematic viscosity of working fluid (m^2/s) +"default" SpdSound - Speed of sound in working fluid (m/s) +"default" Patm - Atmospheric pressure (Pa) [used only when CavitCheck=True] +"default" Pvap - Vapour pressure of working fluid (Pa) [used only when CavitCheck=True] +====== Blade-Element/Momentum Theory Options ====================================================== [unused when Wake_Mod=0 or 3, except for BEM_Mod] +1 BEM_Mod - BEM model {1=legacy NoSweepPitchTwist, 2=polar} (switch) [used for all Wake_Mod to determine output coordinate system] +--- Skew correction +1 Skew_Mod - Skew model {0=No skew model, -1=Remove non-normal component for linearization, 1=skew model active} +False SkewMomCorr - Turn the skew momentum correction on or off [used only when Skew_Mod=1] +default SkewRedistr_Mod - Type of skewed-wake correction model (switch) {0=no redistribution, 1=Glauert/Pitt/Peters, default=1} [used only when Skew_Mod=1] +"default" SkewRedistrFactor - Constant used in Pitt/Peters skewed wake model {or "default" is 15/32*pi} (-) [used only when Skew_Mod=1 and SkewRedistr_Mod=1] +--- BEM algorithm +True TipLoss - Use the Prandtl tip-loss model? (flag) [unused when Wake_Mod=0 or 3] +True HubLoss - Use the Prandtl hub-loss model? (flag) [unused when Wake_Mod=0 or 3] +True TanInd - Include tangential induction in BEMT calculations? (flag) [unused when Wake_Mod=0 or 3] +False AIDrag - Include the drag term in the axial-induction calculation? (flag) [unused when Wake_Mod=0 or 3] +False TIDrag - Include the drag term in the tangential-induction calculation? (flag) [unused when Wake_Mod=0,3 or TanInd=FALSE] +"Default" IndToler - Convergence tolerance for BEMT nonlinear solve residual equation {or "default"} (-) [unused when Wake_Mod=0 or 3] +100 MaxIter - Maximum number of iteration steps (-) [unused when Wake_Mod=0] +--- Shear correction +False SectAvg - Use sector averaging (flag) +1 SectAvgWeighting - Weighting function for sector average {1=Uniform, default=1} within a sector centered on the blade (switch) [used only when SectAvg=True] +default SectAvgNPoints - Number of points per sectors (-) {default=5} [used only when SectAvg=True] +default SectAvgPsiBwd - Backward azimuth relative to blade where the sector starts (<=0) {default=-60} (deg) [used only when SectAvg=True] +default SectAvgPsiFwd - Forward azimuth relative to blade where the sector ends (>=0) {default=60} (deg) [used only when SectAvg=True] +--- Dynamic wake/inflow +0 DBEMT_Mod - Type of dynamic BEMT (DBEMT) model {0=No Dynamic Wake, -1=Frozen Wake for linearization, 1:constant tau1, 2=time-dependent tau1, 3=constant tau1 with continuous formulation} (-) +4 tau1_const - Time constant for DBEMT (s) [used only when DBEMT_Mod=1 or 3] +====== OLAF -- cOnvecting LAgrangian Filaments (Free Vortex Wake) Theory Options ================== [used only when Wake_Mod=3] +"unused" OLAFInputFileName - Input file for OLAF [used only when Wake_Mod=3] +====== Unsteady Airfoil Aerodynamics Options ==================================================== +False AoA34 - Sample the angle of attack (AoA) at the 3/4 chord or the AC point {default=True} [always used] +0 UA_Mod - Unsteady Aero Model Switch (switch) {0=Quasi-steady (no UA), 2=B-L Gonzalez, 3=B-L Minnema/Pierce, 4=B-L HGM 4-states, 5=B-L HGM+vortex 5 states, 6=Oye, 7=Boeing-Vertol} +True FLookup - Flag to indicate whether a lookup for f' will be calculated (TRUE) or whether best-fit exponential equations will be used (FALSE); if FALSE S1-S4 must be provided in airfoil input files (flag) [used only when UA_Mod>0] +3 IntegrationMethod - Switch to indicate which integration method UA uses (1=RK4, 2=AB4, 3=ABM4, 4=BDF2) +0 UAStartRad - Starting radius for dynamic stall (fraction of rotor radius [0.0,1.0]) [used only when UA_Mod>0; if line is missing UAStartRad=0] +1 UAEndRad - Ending radius for dynamic stall (fraction of rotor radius [0.0,1.0]) [used only when UA_Mod>0; if line is missing UAEndRad=1] +====== Airfoil Information ========================================================================= + 1 AFTabMod - Interpolation method for multiple airfoil tables {1=1D interpolation on AoA (first table only); 2=2D interpolation on AoA and Re; 3=2D interpolation on AoA and UserProp} (-) + 1 InCol_Alfa - The column in the airfoil tables that contains the angle of attack (-) + 2 InCol_Cl - The column in the airfoil tables that contains the lift coefficient (-) + 3 InCol_Cd - The column in the airfoil tables that contains the drag coefficient (-) + 4 InCol_Cm - The column in the airfoil tables that contains the pitching-moment coefficient; use zero if there is no Cm column (-) + 0 InCol_Cpmin - The column in the airfoil tables that contains the Cpmin coefficient; use zero if there is no Cpmin column (-) + 8 NumAFfiles - Number of airfoil files used (-) +"Airfoils/Cylinder1.dat" AFNames - Airfoil file names (NumAFfiles lines) (quoted strings) +"Airfoils/Cylinder2.dat" +"Airfoils/DU40_A17.dat" +"Airfoils/DU35_A17.dat" +"Airfoils/DU30_A17.dat" +"Airfoils/DU25_A17.dat" +"Airfoils/DU21_A17.dat" +"Airfoils/NACA64_A17.dat" +====== Rotor/Blade Properties ===================================================================== +True UseBlCm - Include aerodynamic pitching moment in calculations? (flag) +"NRELOffshrBsline5MW_AeroDyn_blade.dat" ADBlFile(1) - Name of file containing distributed aerodynamic properties for Blade #1 (-) +"NRELOffshrBsline5MW_AeroDyn_blade.dat" ADBlFile(2) - Name of file containing distributed aerodynamic properties for Blade #2 (-) [unused if NumBl < 2] +"NRELOffshrBsline5MW_AeroDyn_blade.dat" ADBlFile(3) - Name of file containing distributed aerodynamic properties for Blade #3 (-) [unused if NumBl < 3] +====== Hub Properties ============================================================================== [used only when Buoyancy=True] +0.0 VolHub - Hub volume (m^3) +0.0 HubCenBx - Hub center of buoyancy x direction offset (m) +====== Nacelle Properties ========================================================================== [used only when Buoyancy=True] +0.0 VolNac - Nacelle volume (m^3) +0,0,0 NacCenB - Position of nacelle center of buoyancy from yaw bearing in nacelle coordinates (m) +0, 0, 0 NacArea - Projected area of the nacelle in X, Y, Z in the nacelle coordinate system (m^2) +0, 0, 0 NacCd - Drag coefficient for the nacelle areas defined above (-) +0, 0, 0 NacDragAC - Position of aerodynamic center of nacelle drag in nacelle coordinates (m) +====== Tail fin Aerodynamics ======================================================================== +False TFinAero - Calculate tail fin aerodynamics model (flag) +"unused" TFinFile - Input file for tail fin aerodynamics [used only when TFinAero=True] +====== Tower Influence and Aerodynamics ============================================================ [used only when TwrPotent/=0, TwrShadow/=0, TwrAero=True, or Buoyancy=True] + 12 NumTwrNds - Number of tower nodes used in the analysis (-) [used only when TwrPotent/=0, TwrShadow/=0, TwrAero=True, or Buoyancy=True] +TwrElev TwrDiam TwrCd TwrTI TwrCb !TwrTI used only with TwrShadow=2, TwrCb used only with Buoyancy=True +(m) (m) (-) (-) (-) +0.0000000E+00 6.0000000E+00 1.0000000E+00 1.0000000E-01 0.0 +8.5261000E+00 5.7870000E+00 1.0000000E+00 1.0000000E-01 0.0 +1.7053000E+01 5.5740000E+00 1.0000000E+00 1.0000000E-01 0.0 +2.5579000E+01 5.3610000E+00 1.0000000E+00 1.0000000E-01 0.0 +3.4105000E+01 5.1480000E+00 1.0000000E+00 1.0000000E-01 0.0 +4.2633000E+01 4.9350000E+00 1.0000000E+00 1.0000000E-01 0.0 +5.1158000E+01 4.7220000E+00 1.0000000E+00 1.0000000E-01 0.0 +5.9685000E+01 4.5090000E+00 1.0000000E+00 1.0000000E-01 0.0 +6.8211000E+01 4.2960000E+00 1.0000000E+00 1.0000000E-01 0.0 +7.6738000E+01 4.0830000E+00 1.0000000E+00 1.0000000E-01 0.0 +8.5268000E+01 3.8700000E+00 1.0000000E+00 1.0000000E-01 0.0 +8.7600000E+01 3.8700000E+00 1.0000000E+00 1.0000000E-01 0.0 +====== Outputs ==================================================================================== +False SumPrint - Generate a summary file listing input options and interpolated properties to ".AD.sum"? (flag) + 0 NBlOuts - Number of blade node outputs [0 - 9] (-) + 1, 9, 19 BlOutNd - Blade nodes whose values will be output (-) + 0 NTwOuts - Number of tower node outputs [0 - 9] (-) + 1, 2, 6 TwOutNd - Tower nodes whose values will be output (-) + OutList - The next line(s) contains a list of output parameters. See OutListParameters.xlsx for a listing of available output channels, (-) +END of OutList section (the word "END" must appear in the first 3 columns of the last OutList line) +---------------------- NODE OUTPUTS -------------------------------------------- +0 BldNd_BladesOut - Number of blades to output all node information at. Up to number of blades on turbine. (-) +ALL BldNd_BlOutNd - Specify a portion of the nodes to output. {"ALL", "Tip", "Root", or a list of node numbers} (-) + OutList_Nodal - The next line(s) contains a list of output parameters. See OutListParameters.xlsx for a listing of available output channels, (-) + +END (the word "END" must appear in the first 3 columns of this last OutList line in the optional nodal output section) +==================================================================================================== diff --git a/examples/FAST.Farm_interface/inputs/FFFiles/NRELOffshrBsline5MW_Onshore_ElastoDyn.T1_mod.dat b/examples/FAST.Farm_interface/inputs/FFFiles/NRELOffshrBsline5MW_Onshore_ElastoDyn.T1_mod.dat new file mode 100644 index 00000000..e7292c0b --- /dev/null +++ b/examples/FAST.Farm_interface/inputs/FFFiles/NRELOffshrBsline5MW_Onshore_ElastoDyn.T1_mod.dat @@ -0,0 +1,170 @@ +------- ELASTODYN for OpenFAST INPUT FILE ------------------------------------------- +NREL MW - Baseline Wind Turbine for Use in Offshore Analysis. Properties from Dutch Offshore Wind Energy Converter (DOWEC) 6MW Pre-Design (10046_009.pdf) and REpower 5M 5MW (5m_uk.pdf) +---------------------- SIMULATION CONTROL -------------------------------------- +False Echo - Echo input data to ".ech" (flag) +3 Method - Integration method: {1: RK4, 2: AB4, or 3: ABM4} (-) +"DEFAULT" DT - Integration time step (s) +---------------------- DEGREES OF FREEDOM -------------------------------------- +True FlapDOF1 - First flapwise blade mode DOF (flag) +True FlapDOF2 - Second flapwise blade mode DOF (flag) +True EdgeDOF - First edgewise blade mode DOF (flag) +False TeetDOF - Rotor-teeter DOF (flag) [unused for 3 blades] +True DrTrDOF - Drivetrain rotational-flexibility DOF (flag) +True GenDOF - Generator DOF (flag) +True YawDOF - Yaw DOF (flag) +True TwFADOF1 - First fore-aft tower bending-mode DOF (flag) +True TwFADOF2 - Second fore-aft tower bending-mode DOF (flag) +True TwSSDOF1 - First side-to-side tower bending-mode DOF (flag) +True TwSSDOF2 - Second side-to-side tower bending-mode DOF (flag) +False PtfmSgDOF - Platform horizontal surge translation DOF (flag) +False PtfmSwDOF - Platform horizontal sway translation DOF (flag) +False PtfmHvDOF - Platform vertical heave translation DOF (flag) +False PtfmRDOF - Platform roll tilt rotation DOF (flag) +False PtfmPDOF - Platform pitch tilt rotation DOF (flag) +False PtfmYDOF - Platform yaw rotation DOF (flag) +---------------------- INITIAL CONDITIONS -------------------------------------- +0 OoPDefl - Initial out-of-plane blade-tip displacement (meters) +0 IPDefl - Initial in-plane blade-tip deflection (meters) +0.0 BlPitch(1) - Blade 1 initial pitch (degrees) +0.0 BlPitch(2) - Blade 2 initial pitch (degrees) +0.0 BlPitch(3) - Blade 3 initial pitch (degrees) [unused for 2 blades] +0 TeetDefl - Initial or fixed teeter angle (degrees) [unused for 3 blades] +277 Azimuth - Initial azimuth angle for blade 1 (degrees) +6.087 RotSpeed - Initial or fixed rotor speed (rpm) +0 NacYaw - Initial or fixed nacelle-yaw angle (degrees) +0 TTDspFA - Initial fore-aft tower-top displacement (meters) +0 TTDspSS - Initial side-to-side tower-top displacement (meters) +0 PtfmSurge - Initial or fixed horizontal surge translational displacement of platform (meters) +0 PtfmSway - Initial or fixed horizontal sway translational displacement of platform (meters) +0 PtfmHeave - Initial or fixed vertical heave translational displacement of platform (meters) +0 PtfmRoll - Initial or fixed roll tilt rotational displacement of platform (degrees) +0 PtfmPitch - Initial or fixed pitch tilt rotational displacement of platform (degrees) +0 PtfmYaw - Initial or fixed yaw rotational displacement of platform (degrees) +---------------------- TURBINE CONFIGURATION ----------------------------------- +3 NumBl - Number of blades (-) +63 TipRad - The distance from the rotor apex to the blade tip (meters) +1.5 HubRad - The distance from the rotor apex to the blade root (meters) +-2.5 PreCone(1) - Blade 1 cone angle (degrees) +-2.5 PreCone(2) - Blade 2 cone angle (degrees) +-2.5 PreCone(3) - Blade 3 cone angle (degrees) [unused for 2 blades] +0 HubCM - Distance from rotor apex to hub mass [positive downwind] (meters) +0 UndSling - Undersling length [distance from teeter pin to the rotor apex] (meters) [unused for 3 blades] +0 Delta3 - Delta-3 angle for teetering rotors (degrees) [unused for 3 blades] +0 AzimB1Up - Azimuth value to use for I/O when blade 1 points up (degrees) +-5.0191 OverHang - Distance from yaw axis to rotor apex [3 blades] or teeter pin [2 blades] (meters) +1.912 ShftGagL - Distance from rotor apex [3 blades] or teeter pin [2 blades] to shaft strain gages [positive for upwind rotors] (meters) +-5 ShftTilt - Rotor shaft tilt angle (degrees) +1.9 NacCMxn - Downwind distance from the tower-top to the nacelle CM (meters) +0 NacCMyn - Lateral distance from the tower-top to the nacelle CM (meters) +1.75 NacCMzn - Vertical distance from the tower-top to the nacelle CM (meters) +-3.09528 NcIMUxn - Downwind distance from the tower-top to the nacelle IMU (meters) +0 NcIMUyn - Lateral distance from the tower-top to the nacelle IMU (meters) +2.23336 NcIMUzn - Vertical distance from the tower-top to the nacelle IMU (meters) +1.96256 Twr2Shft - Vertical distance from the tower-top to the rotor shaft (meters) +87.6 TowerHt - Height of tower relative to ground level [onshore], MSL [offshore wind or floating MHK], or seabed [fixed MHK] (meters) +0 TowerBsHt - Height of tower base relative to ground level [onshore], MSL [offshore wind or floating MHK], or seabed [fixed MHK] (meters) +0 PtfmCMxt - Downwind distance from the ground level [onshore], MSL [offshore wind or floating MHK], or seabed [fixed MHK] to the platform CM (meters) +0 PtfmCMyt - Lateral distance from the ground level [onshore], MSL [offshore wind or floating MHK], or seabed [fixed MHK] to the platform CM (meters) +0 PtfmCMzt - Vertical distance from the ground level [onshore], MSL [offshore wind or floating MHK], or seabed [fixed MHK] to the platform CM (meters) +0 PtfmRefzt - Vertical distance from the ground level [onshore], MSL [offshore wind or floating MHK], or seabed [fixed MHK] to the platform reference point (meters) +---------------------- MASS AND INERTIA ---------------------------------------- +0 TipMass(1) - Tip-brake mass, blade 1 (kg) +0 TipMass(2) - Tip-brake mass, blade 2 (kg) +0 TipMass(3) - Tip-brake mass, blade 3 (kg) [unused for 2 blades] +56780 HubMass - Hub mass (kg) +115926 HubIner - Hub inertia about rotor axis [3 blades] or teeter axis [2 blades] (kg m^2) +0 HubIner_Teeter - Hub inertia about teeter axis (2-blades) (kg m^2) +534.116 GenIner - Generator inertia about HSS (kg m^2) +240000 NacMass - Nacelle mass (kg) +2607890.0 NacYIner - Nacelle inertia about yaw axis (kg m^2) +0 YawBrMass - Yaw bearing mass (kg) +0 PtfmMass - Platform mass (kg) +0 PtfmRIner - Platform inertia for roll tilt rotation about the platform CM (kg m^2) +0 PtfmPIner - Platform inertia for pitch tilt rotation about the platform CM (kg m^2) +0 PtfmYIner - Platform inertia for yaw rotation about the platform CM (kg m^2) +0 PtfmXYIner - Platform xy moment of inertia about the platform CM (=-int(xydm)) (kg m^2) +0 PtfmYZIner - Platform yz moment of inertia about the platform CM (=-int(yzdm)) (kg m^2) +0 PtfmXZIner - Platform xz moment of inertia about the platform CM (=-int(xzdm)) (kg m^2) +---------------------- BLADE --------------------------------------------------- +17 BldNodes - Number of blade nodes (per blade) used for analysis (-) +"NRELOffshrBsline5MW_Blade.dat" BldFile(1) - Name of file containing properties for blade 1 (quoted string) +"NRELOffshrBsline5MW_Blade.dat" BldFile(2) - Name of file containing properties for blade 2 (quoted string) +"NRELOffshrBsline5MW_Blade.dat" BldFile(3) - Name of file containing properties for blade 3 (quoted string) [unused for 2 blades] +---------------------- ROTOR-TEETER -------------------------------------------- +0 TeetMod - Rotor-teeter spring/damper model {0: none, 1: standard, 2: user-defined from routine UserTeet} (switch) [unused for 3 blades] +0 TeetDmpP - Rotor-teeter damper position (degrees) [used only for 2 blades and when TeetMod=1] +0 TeetDmp - Rotor-teeter damping constant (N-m/(rad/s)) [used only for 2 blades and when TeetMod=1] +0 TeetCDmp - Rotor-teeter rate-independent Coulomb-damping moment (N-m) [used only for 2 blades and when TeetMod=1] +0 TeetSStP - Rotor-teeter soft-stop position (degrees) [used only for 2 blades and when TeetMod=1] +0 TeetHStP - Rotor-teeter hard-stop position (degrees) [used only for 2 blades and when TeetMod=1] +0 TeetSSSp - Rotor-teeter soft-stop linear-spring constant (N-m/rad) [used only for 2 blades and when TeetMod=1] +0 TeetHSSp - Rotor-teeter hard-stop linear-spring constant (N-m/rad) [used only for 2 blades and when TeetMod=1] +---------------------- YAW-FRICTION -------------------------------------------- + 0 YawFrctMod - Yaw-friction model {0: none, 1: friction independent of yaw-bearing force and bending moment, 2: friction with Coulomb terms depending on yaw-bearing force and bending moment, 3: user defined model} (switch) + 300 M_CSmax - Maximum static Coulomb friction torque (N-m) [M_CSmax when YawFrctMod=1; |Fz|*M_CSmax when YawFrctMod=2 and Fz<0] + 0 M_FCSmax - Maximum static Coulomb friction torque proportional to yaw bearing shear force (N-m) [sqrt(Fx^2+Fy^2)*M_FCSmax; only used when YawFrctMod=2] + 0 M_MCSmax - Maximum static Coulomb friction torque proportional to yaw bearing bending moment (N-m) [sqrt(Mx^2+My^2)*M_MCSmax; only used when YawFrctMod=2] + 40 M_CD - Dynamic Coulomb friction moment (N-m) [M_CD when YawFrctMod=1; |Fz|*M_CD when YawFrctMod=2 and Fz<0] + 0 M_FCD - Dynamic Coulomb friction moment proportional to yaw bearing shear force (N-m) [sqrt(Fx^2+Fy^2)*M_FCD; only used when YawFrctMod=2] + 0 M_MCD - Dynamic Coulomb friction moment proportional to yaw bearing bending moment (N-m) [sqrt(Mx^2+My^2)*M_MCD; only used when YawFrctMod=2] + 0 sig_v - Linear viscous friction coefficient (N-m/(rad/s)) + 0 sig_v2 - Quadratic viscous friction coefficient (N-m/(rad/s)^2) + 0 OmgCut - Yaw angular velocity cutoff below which viscous friction is linearized (rad/s) +---------------------- DRIVETRAIN ---------------------------------------------- +100 GBoxEff - Gearbox efficiency (%) +97 GBRatio - Gearbox ratio (-) +867637000.0 DTTorSpr - Drivetrain torsional spring (N-m/rad) +6215000.0 DTTorDmp - Drivetrain torsional damper (N-m/(rad/s)) +---------------------- FURLING ------------------------------------------------- +False Furling - Read in additional model properties for furling turbine (flag) [must currently be FALSE) +"unused" FurlFile - Name of file containing furling properties (quoted string) [unused when Furling=False] +---------------------- TOWER --------------------------------------------------- +20 TwrNodes - Number of tower nodes used for analysis (-) +"NRELOffshrBsline5MW_Onshore_ElastoDyn_Tower.dat" TwrFile - Name of file containing tower properties (quoted string) +---------------------- OUTPUT -------------------------------------------------- +False SumPrint - Print summary data to ".sum" (flag) +1 OutFile - Switch to determine where output will be placed: {1: in module output file only; 2: in glue code output file only; 3: both} (currently unused) +True TabDelim - Use tab delimiters in text tabular output file? (flag) (currently unused) +"ES10.3E2" OutFmt - Format used for text tabular output (except time). Resulting field should be 10 characters. (quoted string) (currently unused) +0 TStart - Time to begin tabular output (s) (currently unused) +1 DecFact - Decimation factor for tabular output {1: output every time step} (-) (currently unused) +0 NTwGages - Number of tower nodes that have strain gages for output [0 to 9] (-) +10, 19, 28 TwrGagNd - List of tower nodes that have strain gages [1 to TwrNodes] (-) [unused if NTwGages=0] +3 NBlGages - Number of blade nodes that have strain gages for output [0 to 9] (-) +5, 9, 13 BldGagNd - List of blade nodes that have strain gages [1 to BldNodes] (-) [unused if NBlGages=0] + OutList The next line(s) contains a list of output parameters. See OutListParameters.xlsx for a listing of available output channels, (-) +"OoPDefl1" - Blade 1 out-of-plane and in-plane deflections and tip twist +"IPDefl1" - Blade 1 out-of-plane and in-plane deflections and tip twist +"TwstDefl1" - Blade 1 out-of-plane and in-plane deflections and tip twist +"BldPitch1" - Blade 1 pitch angle +"Azimuth" - Blade 1 azimuth angle +"RotSpeed" - Low-speed shaft and high-speed shaft speeds +"GenSpeed" - Low-speed shaft and high-speed shaft speeds +"TTDspFA" - Tower fore-aft and side-to-side displacements and top twist +"TTDspSS" - Tower fore-aft and side-to-side displacements and top twist +"TTDspTwst" - Tower fore-aft and side-to-side displacements and top twist +"Spn2MLxb1" - Blade 1 local edgewise and flapwise bending moments at span station 2 (approx. 50% span) +"Spn2MLyb1" - Blade 1 local edgewise and flapwise bending moments at span station 2 (approx. 50% span) +"RootFxb1" - Out-of-plane shear, in-plane shear, and axial forces at the root of blade 1 +"RootFyb1" - Out-of-plane shear, in-plane shear, and axial forces at the root of blade 1 +"RootFzb1" - Out-of-plane shear, in-plane shear, and axial forces at the root of blade 1 +"RootMxb1" - In-plane bending, out-of-plane bending, and pitching moments at the root of blade 1 +"RootMyb1" - In-plane bending, out-of-plane bending, and pitching moments at the root of blade 1 +"RootMzb1" - In-plane bending, out-of-plane bending, and pitching moments at the root of blade 1 +"RotTorq" - Rotor torque and low-speed shaft 0- and 90-bending moments at the main bearing +"LSSGagMya" - Rotor torque and low-speed shaft 0- and 90-bending moments at the main bearing +"LSSGagMza" - Rotor torque and low-speed shaft 0- and 90-bending moments at the main bearing +"YawBrFxp" - Fore-aft shear, side-to-side shear, and vertical forces at the top of the tower (not rotating with nacelle yaw) +"YawBrFyp" - Fore-aft shear, side-to-side shear, and vertical forces at the top of the tower (not rotating with nacelle yaw) +"YawBrFzp" - Fore-aft shear, side-to-side shear, and vertical forces at the top of the tower (not rotating with nacelle yaw) +"YawBrMxp" - Side-to-side bending, fore-aft bending, and yaw moments at the top of the tower (not rotating with nacelle yaw) +"YawBrMyp" - Side-to-side bending, fore-aft bending, and yaw moments at the top of the tower (not rotating with nacelle yaw) +"YawBrMzp" - Side-to-side bending, fore-aft bending, and yaw moments at the top of the tower (not rotating with nacelle yaw) +"TwrBsFxt" - Fore-aft shear, side-to-side shear, and vertical forces at the base of the tower (mudline) +"TwrBsFyt" - Fore-aft shear, side-to-side shear, and vertical forces at the base of the tower (mudline) +"TwrBsFzt" - Fore-aft shear, side-to-side shear, and vertical forces at the base of the tower (mudline) +"TwrBsMxt" - Side-to-side bending, fore-aft bending, and yaw moments at the base of the tower (mudline) +"TwrBsMyt" - Side-to-side bending, fore-aft bending, and yaw moments at the base of the tower (mudline) +"TwrBsMzt" - Side-to-side bending, fore-aft bending, and yaw moments at the base of the tower (mudline) +END +--------------------------------------------------------------------------------------- \ No newline at end of file diff --git a/examples/FAST.Farm_interface/inputs/FFFiles/NRELOffshrBsline5MW_Onshore_ElastoDyn.T2_mod.dat b/examples/FAST.Farm_interface/inputs/FFFiles/NRELOffshrBsline5MW_Onshore_ElastoDyn.T2_mod.dat new file mode 100644 index 00000000..1aa85321 --- /dev/null +++ b/examples/FAST.Farm_interface/inputs/FFFiles/NRELOffshrBsline5MW_Onshore_ElastoDyn.T2_mod.dat @@ -0,0 +1,170 @@ +------- ELASTODYN for OpenFAST INPUT FILE ------------------------------------------- +NREL MW - Baseline Wind Turbine for Use in Offshore Analysis. Properties from Dutch Offshore Wind Energy Converter (DOWEC) 6MW Pre-Design (10046_009.pdf) and REpower 5M 5MW (5m_uk.pdf) +---------------------- SIMULATION CONTROL -------------------------------------- +False Echo - Echo input data to ".ech" (flag) +3 Method - Integration method: {1: RK4, 2: AB4, or 3: ABM4} (-) +"DEFAULT" DT - Integration time step (s) +---------------------- DEGREES OF FREEDOM -------------------------------------- +True FlapDOF1 - First flapwise blade mode DOF (flag) +True FlapDOF2 - Second flapwise blade mode DOF (flag) +True EdgeDOF - First edgewise blade mode DOF (flag) +False TeetDOF - Rotor-teeter DOF (flag) [unused for 3 blades] +True DrTrDOF - Drivetrain rotational-flexibility DOF (flag) +True GenDOF - Generator DOF (flag) +True YawDOF - Yaw DOF (flag) +True TwFADOF1 - First fore-aft tower bending-mode DOF (flag) +True TwFADOF2 - Second fore-aft tower bending-mode DOF (flag) +True TwSSDOF1 - First side-to-side tower bending-mode DOF (flag) +True TwSSDOF2 - Second side-to-side tower bending-mode DOF (flag) +False PtfmSgDOF - Platform horizontal surge translation DOF (flag) +False PtfmSwDOF - Platform horizontal sway translation DOF (flag) +False PtfmHvDOF - Platform vertical heave translation DOF (flag) +False PtfmRDOF - Platform roll tilt rotation DOF (flag) +False PtfmPDOF - Platform pitch tilt rotation DOF (flag) +False PtfmYDOF - Platform yaw rotation DOF (flag) +---------------------- INITIAL CONDITIONS -------------------------------------- +0 OoPDefl - Initial out-of-plane blade-tip displacement (meters) +0 IPDefl - Initial in-plane blade-tip deflection (meters) +0.0 BlPitch(1) - Blade 1 initial pitch (degrees) +0.0 BlPitch(2) - Blade 2 initial pitch (degrees) +0.0 BlPitch(3) - Blade 3 initial pitch (degrees) [unused for 2 blades] +0 TeetDefl - Initial or fixed teeter angle (degrees) [unused for 3 blades] +256 Azimuth - Initial azimuth angle for blade 1 (degrees) +6.087 RotSpeed - Initial or fixed rotor speed (rpm) +0 NacYaw - Initial or fixed nacelle-yaw angle (degrees) +0 TTDspFA - Initial fore-aft tower-top displacement (meters) +0 TTDspSS - Initial side-to-side tower-top displacement (meters) +0 PtfmSurge - Initial or fixed horizontal surge translational displacement of platform (meters) +0 PtfmSway - Initial or fixed horizontal sway translational displacement of platform (meters) +0 PtfmHeave - Initial or fixed vertical heave translational displacement of platform (meters) +0 PtfmRoll - Initial or fixed roll tilt rotational displacement of platform (degrees) +0 PtfmPitch - Initial or fixed pitch tilt rotational displacement of platform (degrees) +0 PtfmYaw - Initial or fixed yaw rotational displacement of platform (degrees) +---------------------- TURBINE CONFIGURATION ----------------------------------- +3 NumBl - Number of blades (-) +63 TipRad - The distance from the rotor apex to the blade tip (meters) +1.5 HubRad - The distance from the rotor apex to the blade root (meters) +-2.5 PreCone(1) - Blade 1 cone angle (degrees) +-2.5 PreCone(2) - Blade 2 cone angle (degrees) +-2.5 PreCone(3) - Blade 3 cone angle (degrees) [unused for 2 blades] +0 HubCM - Distance from rotor apex to hub mass [positive downwind] (meters) +0 UndSling - Undersling length [distance from teeter pin to the rotor apex] (meters) [unused for 3 blades] +0 Delta3 - Delta-3 angle for teetering rotors (degrees) [unused for 3 blades] +0 AzimB1Up - Azimuth value to use for I/O when blade 1 points up (degrees) +-5.0191 OverHang - Distance from yaw axis to rotor apex [3 blades] or teeter pin [2 blades] (meters) +1.912 ShftGagL - Distance from rotor apex [3 blades] or teeter pin [2 blades] to shaft strain gages [positive for upwind rotors] (meters) +-5 ShftTilt - Rotor shaft tilt angle (degrees) +1.9 NacCMxn - Downwind distance from the tower-top to the nacelle CM (meters) +0 NacCMyn - Lateral distance from the tower-top to the nacelle CM (meters) +1.75 NacCMzn - Vertical distance from the tower-top to the nacelle CM (meters) +-3.09528 NcIMUxn - Downwind distance from the tower-top to the nacelle IMU (meters) +0 NcIMUyn - Lateral distance from the tower-top to the nacelle IMU (meters) +2.23336 NcIMUzn - Vertical distance from the tower-top to the nacelle IMU (meters) +1.96256 Twr2Shft - Vertical distance from the tower-top to the rotor shaft (meters) +87.6 TowerHt - Height of tower relative to ground level [onshore], MSL [offshore wind or floating MHK], or seabed [fixed MHK] (meters) +0 TowerBsHt - Height of tower base relative to ground level [onshore], MSL [offshore wind or floating MHK], or seabed [fixed MHK] (meters) +0 PtfmCMxt - Downwind distance from the ground level [onshore], MSL [offshore wind or floating MHK], or seabed [fixed MHK] to the platform CM (meters) +0 PtfmCMyt - Lateral distance from the ground level [onshore], MSL [offshore wind or floating MHK], or seabed [fixed MHK] to the platform CM (meters) +0 PtfmCMzt - Vertical distance from the ground level [onshore], MSL [offshore wind or floating MHK], or seabed [fixed MHK] to the platform CM (meters) +0 PtfmRefzt - Vertical distance from the ground level [onshore], MSL [offshore wind or floating MHK], or seabed [fixed MHK] to the platform reference point (meters) +---------------------- MASS AND INERTIA ---------------------------------------- +0 TipMass(1) - Tip-brake mass, blade 1 (kg) +0 TipMass(2) - Tip-brake mass, blade 2 (kg) +0 TipMass(3) - Tip-brake mass, blade 3 (kg) [unused for 2 blades] +56780 HubMass - Hub mass (kg) +115926 HubIner - Hub inertia about rotor axis [3 blades] or teeter axis [2 blades] (kg m^2) +0 HubIner_Teeter - Hub inertia about teeter axis (2-blades) (kg m^2) +534.116 GenIner - Generator inertia about HSS (kg m^2) +240000 NacMass - Nacelle mass (kg) +2607890.0 NacYIner - Nacelle inertia about yaw axis (kg m^2) +0 YawBrMass - Yaw bearing mass (kg) +0 PtfmMass - Platform mass (kg) +0 PtfmRIner - Platform inertia for roll tilt rotation about the platform CM (kg m^2) +0 PtfmPIner - Platform inertia for pitch tilt rotation about the platform CM (kg m^2) +0 PtfmYIner - Platform inertia for yaw rotation about the platform CM (kg m^2) + 0 PtfmXYIner - Platform xy moment of inertia about the platform CM (=-int(xydm)) (kg m^2) + 0 PtfmYZIner - Platform yz moment of inertia about the platform CM (=-int(yzdm)) (kg m^2) + 0 PtfmXZIner - Platform xz moment of inertia about the platform CM (=-int(xzdm)) (kg m^2) +---------------------- BLADE --------------------------------------------------- +17 BldNodes - Number of blade nodes (per blade) used for analysis (-) +"NRELOffshrBsline5MW_Blade.dat" BldFile(1) - Name of file containing properties for blade 1 (quoted string) +"NRELOffshrBsline5MW_Blade.dat" BldFile(2) - Name of file containing properties for blade 2 (quoted string) +"NRELOffshrBsline5MW_Blade.dat" BldFile(3) - Name of file containing properties for blade 3 (quoted string) [unused for 2 blades] +---------------------- ROTOR-TEETER -------------------------------------------- +0 TeetMod - Rotor-teeter spring/damper model {0: none, 1: standard, 2: user-defined from routine UserTeet} (switch) [unused for 3 blades] +0 TeetDmpP - Rotor-teeter damper position (degrees) [used only for 2 blades and when TeetMod=1] +0 TeetDmp - Rotor-teeter damping constant (N-m/(rad/s)) [used only for 2 blades and when TeetMod=1] +0 TeetCDmp - Rotor-teeter rate-independent Coulomb-damping moment (N-m) [used only for 2 blades and when TeetMod=1] +0 TeetSStP - Rotor-teeter soft-stop position (degrees) [used only for 2 blades and when TeetMod=1] +0 TeetHStP - Rotor-teeter hard-stop position (degrees) [used only for 2 blades and when TeetMod=1] +0 TeetSSSp - Rotor-teeter soft-stop linear-spring constant (N-m/rad) [used only for 2 blades and when TeetMod=1] +0 TeetHSSp - Rotor-teeter hard-stop linear-spring constant (N-m/rad) [used only for 2 blades and when TeetMod=1] +---------------------- YAW-FRICTION -------------------------------------------- + 0 YawFrctMod - Yaw-friction model {0: none, 1: friction independent of yaw-bearing force and bending moment, 2: friction with Coulomb terms depending on yaw-bearing force and bending moment, 3: user defined model} (switch) + 300 M_CSmax - Maximum static Coulomb friction torque (N-m) [M_CSmax when YawFrctMod=1; |Fz|*M_CSmax when YawFrctMod=2 and Fz<0] + 0 M_FCSmax - Maximum static Coulomb friction torque proportional to yaw bearing shear force (N-m) [sqrt(Fx^2+Fy^2)*M_FCSmax; only used when YawFrctMod=2] + 0 M_MCSmax - Maximum static Coulomb friction torque proportional to yaw bearing bending moment (N-m) [sqrt(Mx^2+My^2)*M_MCSmax; only used when YawFrctMod=2] + 40 M_CD - Dynamic Coulomb friction moment (N-m) [M_CD when YawFrctMod=1; |Fz|*M_CD when YawFrctMod=2 and Fz<0] + 0 M_FCD - Dynamic Coulomb friction moment proportional to yaw bearing shear force (N-m) [sqrt(Fx^2+Fy^2)*M_FCD; only used when YawFrctMod=2] + 0 M_MCD - Dynamic Coulomb friction moment proportional to yaw bearing bending moment (N-m) [sqrt(Mx^2+My^2)*M_MCD; only used when YawFrctMod=2] + 0 sig_v - Linear viscous friction coefficient (N-m/(rad/s)) + 0 sig_v2 - Quadratic viscous friction coefficient (N-m/(rad/s)^2) + 0 OmgCut - Yaw angular velocity cutoff below which viscous friction is linearized (rad/s) +---------------------- DRIVETRAIN ---------------------------------------------- +100 GBoxEff - Gearbox efficiency (%) +97 GBRatio - Gearbox ratio (-) +867637000.0 DTTorSpr - Drivetrain torsional spring (N-m/rad) +6215000.0 DTTorDmp - Drivetrain torsional damper (N-m/(rad/s)) +---------------------- FURLING ------------------------------------------------- +False Furling - Read in additional model properties for furling turbine (flag) [must currently be FALSE) +"unused" FurlFile - Name of file containing furling properties (quoted string) [unused when Furling=False] +---------------------- TOWER --------------------------------------------------- +20 TwrNodes - Number of tower nodes used for analysis (-) +"NRELOffshrBsline5MW_Onshore_ElastoDyn_Tower.dat" TwrFile - Name of file containing tower properties (quoted string) +---------------------- OUTPUT -------------------------------------------------- +False SumPrint - Print summary data to ".sum" (flag) +1 OutFile - Switch to determine where output will be placed: {1: in module output file only; 2: in glue code output file only; 3: both} (currently unused) +True TabDelim - Use tab delimiters in text tabular output file? (flag) (currently unused) +"ES10.3E2" OutFmt - Format used for text tabular output (except time). Resulting field should be 10 characters. (quoted string) (currently unused) +0 TStart - Time to begin tabular output (s) (currently unused) +1 DecFact - Decimation factor for tabular output {1: output every time step} (-) (currently unused) +0 NTwGages - Number of tower nodes that have strain gages for output [0 to 9] (-) +10, 19, 28 TwrGagNd - List of tower nodes that have strain gages [1 to TwrNodes] (-) [unused if NTwGages=0] +3 NBlGages - Number of blade nodes that have strain gages for output [0 to 9] (-) +5, 9, 13 BldGagNd - List of blade nodes that have strain gages [1 to BldNodes] (-) [unused if NBlGages=0] + OutList The next line(s) contains a list of output parameters. See OutListParameters.xlsx for a listing of available output channels, (-) +"OoPDefl1" - Blade 1 out-of-plane and in-plane deflections and tip twist +"IPDefl1" - Blade 1 out-of-plane and in-plane deflections and tip twist +"TwstDefl1" - Blade 1 out-of-plane and in-plane deflections and tip twist +"BldPitch1" - Blade 1 pitch angle +"Azimuth" - Blade 1 azimuth angle +"RotSpeed" - Low-speed shaft and high-speed shaft speeds +"GenSpeed" - Low-speed shaft and high-speed shaft speeds +"TTDspFA" - Tower fore-aft and side-to-side displacements and top twist +"TTDspSS" - Tower fore-aft and side-to-side displacements and top twist +"TTDspTwst" - Tower fore-aft and side-to-side displacements and top twist +"Spn2MLxb1" - Blade 1 local edgewise and flapwise bending moments at span station 2 (approx. 50% span) +"Spn2MLyb1" - Blade 1 local edgewise and flapwise bending moments at span station 2 (approx. 50% span) +"RootFxb1" - Out-of-plane shear, in-plane shear, and axial forces at the root of blade 1 +"RootFyb1" - Out-of-plane shear, in-plane shear, and axial forces at the root of blade 1 +"RootFzb1" - Out-of-plane shear, in-plane shear, and axial forces at the root of blade 1 +"RootMxb1" - In-plane bending, out-of-plane bending, and pitching moments at the root of blade 1 +"RootMyb1" - In-plane bending, out-of-plane bending, and pitching moments at the root of blade 1 +"RootMzb1" - In-plane bending, out-of-plane bending, and pitching moments at the root of blade 1 +"RotTorq" - Rotor torque and low-speed shaft 0- and 90-bending moments at the main bearing +"LSSGagMya" - Rotor torque and low-speed shaft 0- and 90-bending moments at the main bearing +"LSSGagMza" - Rotor torque and low-speed shaft 0- and 90-bending moments at the main bearing +"YawBrFxp" - Fore-aft shear, side-to-side shear, and vertical forces at the top of the tower (not rotating with nacelle yaw) +"YawBrFyp" - Fore-aft shear, side-to-side shear, and vertical forces at the top of the tower (not rotating with nacelle yaw) +"YawBrFzp" - Fore-aft shear, side-to-side shear, and vertical forces at the top of the tower (not rotating with nacelle yaw) +"YawBrMxp" - Side-to-side bending, fore-aft bending, and yaw moments at the top of the tower (not rotating with nacelle yaw) +"YawBrMyp" - Side-to-side bending, fore-aft bending, and yaw moments at the top of the tower (not rotating with nacelle yaw) +"YawBrMzp" - Side-to-side bending, fore-aft bending, and yaw moments at the top of the tower (not rotating with nacelle yaw) +"TwrBsFxt" - Fore-aft shear, side-to-side shear, and vertical forces at the base of the tower (mudline) +"TwrBsFyt" - Fore-aft shear, side-to-side shear, and vertical forces at the base of the tower (mudline) +"TwrBsFzt" - Fore-aft shear, side-to-side shear, and vertical forces at the base of the tower (mudline) +"TwrBsMxt" - Side-to-side bending, fore-aft bending, and yaw moments at the base of the tower (mudline) +"TwrBsMyt" - Side-to-side bending, fore-aft bending, and yaw moments at the base of the tower (mudline) +"TwrBsMzt" - Side-to-side bending, fore-aft bending, and yaw moments at the base of the tower (mudline) +END +--------------------------------------------------------------------------------------- \ No newline at end of file diff --git a/examples/FAST.Farm_interface/inputs/FFFiles/NRELOffshrBsline5MW_Onshore_ElastoDyn.T3_mod.dat b/examples/FAST.Farm_interface/inputs/FFFiles/NRELOffshrBsline5MW_Onshore_ElastoDyn.T3_mod.dat new file mode 100644 index 00000000..d83bac0f --- /dev/null +++ b/examples/FAST.Farm_interface/inputs/FFFiles/NRELOffshrBsline5MW_Onshore_ElastoDyn.T3_mod.dat @@ -0,0 +1,170 @@ +------- ELASTODYN for OpenFAST INPUT FILE ------------------------------------------- +NREL MW - Baseline Wind Turbine for Use in Offshore Analysis. Properties from Dutch Offshore Wind Energy Converter (DOWEC) 6MW Pre-Design (10046_009.pdf) and REpower 5M 5MW (5m_uk.pdf) +---------------------- SIMULATION CONTROL -------------------------------------- +False Echo - Echo input data to ".ech" (flag) +3 Method - Integration method: {1: RK4, 2: AB4, or 3: ABM4} (-) +"DEFAULT" DT - Integration time step (s) +---------------------- DEGREES OF FREEDOM -------------------------------------- +True FlapDOF1 - First flapwise blade mode DOF (flag) +True FlapDOF2 - Second flapwise blade mode DOF (flag) +True EdgeDOF - First edgewise blade mode DOF (flag) +False TeetDOF - Rotor-teeter DOF (flag) [unused for 3 blades] +True DrTrDOF - Drivetrain rotational-flexibility DOF (flag) +True GenDOF - Generator DOF (flag) +True YawDOF - Yaw DOF (flag) +True TwFADOF1 - First fore-aft tower bending-mode DOF (flag) +True TwFADOF2 - Second fore-aft tower bending-mode DOF (flag) +True TwSSDOF1 - First side-to-side tower bending-mode DOF (flag) +True TwSSDOF2 - Second side-to-side tower bending-mode DOF (flag) +False PtfmSgDOF - Platform horizontal surge translation DOF (flag) +False PtfmSwDOF - Platform horizontal sway translation DOF (flag) +False PtfmHvDOF - Platform vertical heave translation DOF (flag) +False PtfmRDOF - Platform roll tilt rotation DOF (flag) +False PtfmPDOF - Platform pitch tilt rotation DOF (flag) +False PtfmYDOF - Platform yaw rotation DOF (flag) +---------------------- INITIAL CONDITIONS -------------------------------------- +0 OoPDefl - Initial out-of-plane blade-tip displacement (meters) +0 IPDefl - Initial in-plane blade-tip deflection (meters) +0.0 BlPitch(1) - Blade 1 initial pitch (degrees) +0.0 BlPitch(2) - Blade 2 initial pitch (degrees) +0.0 BlPitch(3) - Blade 3 initial pitch (degrees) [unused for 2 blades] +0 TeetDefl - Initial or fixed teeter angle (degrees) [unused for 3 blades] +351 Azimuth - Initial azimuth angle for blade 1 (degrees) +6.087 RotSpeed - Initial or fixed rotor speed (rpm) +0 NacYaw - Initial or fixed nacelle-yaw angle (degrees) +0 TTDspFA - Initial fore-aft tower-top displacement (meters) +0 TTDspSS - Initial side-to-side tower-top displacement (meters) +0 PtfmSurge - Initial or fixed horizontal surge translational displacement of platform (meters) +0 PtfmSway - Initial or fixed horizontal sway translational displacement of platform (meters) +0 PtfmHeave - Initial or fixed vertical heave translational displacement of platform (meters) +0 PtfmRoll - Initial or fixed roll tilt rotational displacement of platform (degrees) +0 PtfmPitch - Initial or fixed pitch tilt rotational displacement of platform (degrees) +0 PtfmYaw - Initial or fixed yaw rotational displacement of platform (degrees) +---------------------- TURBINE CONFIGURATION ----------------------------------- +3 NumBl - Number of blades (-) +63 TipRad - The distance from the rotor apex to the blade tip (meters) +1.5 HubRad - The distance from the rotor apex to the blade root (meters) +-2.5 PreCone(1) - Blade 1 cone angle (degrees) +-2.5 PreCone(2) - Blade 2 cone angle (degrees) +-2.5 PreCone(3) - Blade 3 cone angle (degrees) [unused for 2 blades] +0 HubCM - Distance from rotor apex to hub mass [positive downwind] (meters) +0 UndSling - Undersling length [distance from teeter pin to the rotor apex] (meters) [unused for 3 blades] +0 Delta3 - Delta-3 angle for teetering rotors (degrees) [unused for 3 blades] +0 AzimB1Up - Azimuth value to use for I/O when blade 1 points up (degrees) +-5.0191 OverHang - Distance from yaw axis to rotor apex [3 blades] or teeter pin [2 blades] (meters) +1.912 ShftGagL - Distance from rotor apex [3 blades] or teeter pin [2 blades] to shaft strain gages [positive for upwind rotors] (meters) +-5 ShftTilt - Rotor shaft tilt angle (degrees) +1.9 NacCMxn - Downwind distance from the tower-top to the nacelle CM (meters) +0 NacCMyn - Lateral distance from the tower-top to the nacelle CM (meters) +1.75 NacCMzn - Vertical distance from the tower-top to the nacelle CM (meters) +-3.09528 NcIMUxn - Downwind distance from the tower-top to the nacelle IMU (meters) +0 NcIMUyn - Lateral distance from the tower-top to the nacelle IMU (meters) +2.23336 NcIMUzn - Vertical distance from the tower-top to the nacelle IMU (meters) +1.96256 Twr2Shft - Vertical distance from the tower-top to the rotor shaft (meters) +87.6 TowerHt - Height of tower relative to ground level [onshore], MSL [offshore wind or floating MHK], or seabed [fixed MHK] (meters) +0 TowerBsHt - Height of tower base relative to ground level [onshore], MSL [offshore wind or floating MHK], or seabed [fixed MHK] (meters) +0 PtfmCMxt - Downwind distance from the ground level [onshore], MSL [offshore wind or floating MHK], or seabed [fixed MHK] to the platform CM (meters) +0 PtfmCMyt - Lateral distance from the ground level [onshore], MSL [offshore wind or floating MHK], or seabed [fixed MHK] to the platform CM (meters) +0 PtfmCMzt - Vertical distance from the ground level [onshore], MSL [offshore wind or floating MHK], or seabed [fixed MHK] to the platform CM (meters) +0 PtfmRefzt - Vertical distance from the ground level [onshore], MSL [offshore wind or floating MHK], or seabed [fixed MHK] to the platform reference point (meters) +---------------------- MASS AND INERTIA ---------------------------------------- +0 TipMass(1) - Tip-brake mass, blade 1 (kg) +0 TipMass(2) - Tip-brake mass, blade 2 (kg) +0 TipMass(3) - Tip-brake mass, blade 3 (kg) [unused for 2 blades] +56780 HubMass - Hub mass (kg) +115926 HubIner - Hub inertia about rotor axis [3 blades] or teeter axis [2 blades] (kg m^2) +0 HubIner_Teeter - Hub inertia about teeter axis (2-blades) (kg m^2) +534.116 GenIner - Generator inertia about HSS (kg m^2) +240000 NacMass - Nacelle mass (kg) +2607890.0 NacYIner - Nacelle inertia about yaw axis (kg m^2) +0 YawBrMass - Yaw bearing mass (kg) +0 PtfmMass - Platform mass (kg) +0 PtfmRIner - Platform inertia for roll tilt rotation about the platform CM (kg m^2) +0 PtfmPIner - Platform inertia for pitch tilt rotation about the platform CM (kg m^2) +0 PtfmYIner - Platform inertia for yaw rotation about the platform CM (kg m^2) + 0 PtfmXYIner - Platform xy moment of inertia about the platform CM (=-int(xydm)) (kg m^2) + 0 PtfmYZIner - Platform yz moment of inertia about the platform CM (=-int(yzdm)) (kg m^2) + 0 PtfmXZIner - Platform xz moment of inertia about the platform CM (=-int(xzdm)) (kg m^2) +---------------------- BLADE --------------------------------------------------- +17 BldNodes - Number of blade nodes (per blade) used for analysis (-) +"NRELOffshrBsline5MW_Blade.dat" BldFile(1) - Name of file containing properties for blade 1 (quoted string) +"NRELOffshrBsline5MW_Blade.dat" BldFile(2) - Name of file containing properties for blade 2 (quoted string) +"NRELOffshrBsline5MW_Blade.dat" BldFile(3) - Name of file containing properties for blade 3 (quoted string) [unused for 2 blades] +---------------------- ROTOR-TEETER -------------------------------------------- +0 TeetMod - Rotor-teeter spring/damper model {0: none, 1: standard, 2: user-defined from routine UserTeet} (switch) [unused for 3 blades] +0 TeetDmpP - Rotor-teeter damper position (degrees) [used only for 2 blades and when TeetMod=1] +0 TeetDmp - Rotor-teeter damping constant (N-m/(rad/s)) [used only for 2 blades and when TeetMod=1] +0 TeetCDmp - Rotor-teeter rate-independent Coulomb-damping moment (N-m) [used only for 2 blades and when TeetMod=1] +0 TeetSStP - Rotor-teeter soft-stop position (degrees) [used only for 2 blades and when TeetMod=1] +0 TeetHStP - Rotor-teeter hard-stop position (degrees) [used only for 2 blades and when TeetMod=1] +0 TeetSSSp - Rotor-teeter soft-stop linear-spring constant (N-m/rad) [used only for 2 blades and when TeetMod=1] +0 TeetHSSp - Rotor-teeter hard-stop linear-spring constant (N-m/rad) [used only for 2 blades and when TeetMod=1] +---------------------- YAW-FRICTION -------------------------------------------- + 0 YawFrctMod - Yaw-friction model {0: none, 1: friction independent of yaw-bearing force and bending moment, 2: friction with Coulomb terms depending on yaw-bearing force and bending moment, 3: user defined model} (switch) + 300 M_CSmax - Maximum static Coulomb friction torque (N-m) [M_CSmax when YawFrctMod=1; |Fz|*M_CSmax when YawFrctMod=2 and Fz<0] + 0 M_FCSmax - Maximum static Coulomb friction torque proportional to yaw bearing shear force (N-m) [sqrt(Fx^2+Fy^2)*M_FCSmax; only used when YawFrctMod=2] + 0 M_MCSmax - Maximum static Coulomb friction torque proportional to yaw bearing bending moment (N-m) [sqrt(Mx^2+My^2)*M_MCSmax; only used when YawFrctMod=2] + 40 M_CD - Dynamic Coulomb friction moment (N-m) [M_CD when YawFrctMod=1; |Fz|*M_CD when YawFrctMod=2 and Fz<0] + 0 M_FCD - Dynamic Coulomb friction moment proportional to yaw bearing shear force (N-m) [sqrt(Fx^2+Fy^2)*M_FCD; only used when YawFrctMod=2] + 0 M_MCD - Dynamic Coulomb friction moment proportional to yaw bearing bending moment (N-m) [sqrt(Mx^2+My^2)*M_MCD; only used when YawFrctMod=2] + 0 sig_v - Linear viscous friction coefficient (N-m/(rad/s)) + 0 sig_v2 - Quadratic viscous friction coefficient (N-m/(rad/s)^2) + 0 OmgCut - Yaw angular velocity cutoff below which viscous friction is linearized (rad/s) +---------------------- DRIVETRAIN ---------------------------------------------- +100 GBoxEff - Gearbox efficiency (%) +97 GBRatio - Gearbox ratio (-) +867637000.0 DTTorSpr - Drivetrain torsional spring (N-m/rad) +6215000.0 DTTorDmp - Drivetrain torsional damper (N-m/(rad/s)) +---------------------- FURLING ------------------------------------------------- +False Furling - Read in additional model properties for furling turbine (flag) [must currently be FALSE) +"unused" FurlFile - Name of file containing furling properties (quoted string) [unused when Furling=False] +---------------------- TOWER --------------------------------------------------- +20 TwrNodes - Number of tower nodes used for analysis (-) +"NRELOffshrBsline5MW_Onshore_ElastoDyn_Tower.dat" TwrFile - Name of file containing tower properties (quoted string) +---------------------- OUTPUT -------------------------------------------------- +False SumPrint - Print summary data to ".sum" (flag) +1 OutFile - Switch to determine where output will be placed: {1: in module output file only; 2: in glue code output file only; 3: both} (currently unused) +True TabDelim - Use tab delimiters in text tabular output file? (flag) (currently unused) +"ES10.3E2" OutFmt - Format used for text tabular output (except time). Resulting field should be 10 characters. (quoted string) (currently unused) +0 TStart - Time to begin tabular output (s) (currently unused) +1 DecFact - Decimation factor for tabular output {1: output every time step} (-) (currently unused) +0 NTwGages - Number of tower nodes that have strain gages for output [0 to 9] (-) +10, 19, 28 TwrGagNd - List of tower nodes that have strain gages [1 to TwrNodes] (-) [unused if NTwGages=0] +3 NBlGages - Number of blade nodes that have strain gages for output [0 to 9] (-) +5, 9, 13 BldGagNd - List of blade nodes that have strain gages [1 to BldNodes] (-) [unused if NBlGages=0] + OutList The next line(s) contains a list of output parameters. See OutListParameters.xlsx for a listing of available output channels, (-) +"OoPDefl1" - Blade 1 out-of-plane and in-plane deflections and tip twist +"IPDefl1" - Blade 1 out-of-plane and in-plane deflections and tip twist +"TwstDefl1" - Blade 1 out-of-plane and in-plane deflections and tip twist +"BldPitch1" - Blade 1 pitch angle +"Azimuth" - Blade 1 azimuth angle +"RotSpeed" - Low-speed shaft and high-speed shaft speeds +"GenSpeed" - Low-speed shaft and high-speed shaft speeds +"TTDspFA" - Tower fore-aft and side-to-side displacements and top twist +"TTDspSS" - Tower fore-aft and side-to-side displacements and top twist +"TTDspTwst" - Tower fore-aft and side-to-side displacements and top twist +"Spn2MLxb1" - Blade 1 local edgewise and flapwise bending moments at span station 2 (approx. 50% span) +"Spn2MLyb1" - Blade 1 local edgewise and flapwise bending moments at span station 2 (approx. 50% span) +"RootFxb1" - Out-of-plane shear, in-plane shear, and axial forces at the root of blade 1 +"RootFyb1" - Out-of-plane shear, in-plane shear, and axial forces at the root of blade 1 +"RootFzb1" - Out-of-plane shear, in-plane shear, and axial forces at the root of blade 1 +"RootMxb1" - In-plane bending, out-of-plane bending, and pitching moments at the root of blade 1 +"RootMyb1" - In-plane bending, out-of-plane bending, and pitching moments at the root of blade 1 +"RootMzb1" - In-plane bending, out-of-plane bending, and pitching moments at the root of blade 1 +"RotTorq" - Rotor torque and low-speed shaft 0- and 90-bending moments at the main bearing +"LSSGagMya" - Rotor torque and low-speed shaft 0- and 90-bending moments at the main bearing +"LSSGagMza" - Rotor torque and low-speed shaft 0- and 90-bending moments at the main bearing +"YawBrFxp" - Fore-aft shear, side-to-side shear, and vertical forces at the top of the tower (not rotating with nacelle yaw) +"YawBrFyp" - Fore-aft shear, side-to-side shear, and vertical forces at the top of the tower (not rotating with nacelle yaw) +"YawBrFzp" - Fore-aft shear, side-to-side shear, and vertical forces at the top of the tower (not rotating with nacelle yaw) +"YawBrMxp" - Side-to-side bending, fore-aft bending, and yaw moments at the top of the tower (not rotating with nacelle yaw) +"YawBrMyp" - Side-to-side bending, fore-aft bending, and yaw moments at the top of the tower (not rotating with nacelle yaw) +"YawBrMzp" - Side-to-side bending, fore-aft bending, and yaw moments at the top of the tower (not rotating with nacelle yaw) +"TwrBsFxt" - Fore-aft shear, side-to-side shear, and vertical forces at the base of the tower (mudline) +"TwrBsFyt" - Fore-aft shear, side-to-side shear, and vertical forces at the base of the tower (mudline) +"TwrBsFzt" - Fore-aft shear, side-to-side shear, and vertical forces at the base of the tower (mudline) +"TwrBsMxt" - Side-to-side bending, fore-aft bending, and yaw moments at the base of the tower (mudline) +"TwrBsMyt" - Side-to-side bending, fore-aft bending, and yaw moments at the base of the tower (mudline) +"TwrBsMzt" - Side-to-side bending, fore-aft bending, and yaw moments at the base of the tower (mudline) +END +--------------------------------------------------------------------------------------- \ No newline at end of file diff --git a/examples/FAST.Farm_interface/inputs/FFFiles/NRELOffshrBsline5MW_Onshore_ElastoDyn_Tower.dat b/examples/FAST.Farm_interface/inputs/FFFiles/NRELOffshrBsline5MW_Onshore_ElastoDyn_Tower.dat new file mode 100644 index 00000000..664185cb --- /dev/null +++ b/examples/FAST.Farm_interface/inputs/FFFiles/NRELOffshrBsline5MW_Onshore_ElastoDyn_Tower.dat @@ -0,0 +1,54 @@ +------- ELASTODYN V1.00.* TOWER INPUT FILE ------------------------------------- +NREL 5.0 MW offshore baseline tower input properties. +---------------------- TOWER PARAMETERS ---------------------------------------- + 11 NTwInpSt - Number of input stations to specify tower geometry + 1 TwrFADmp(1) - Tower 1st fore-aft mode structural damping ratio (%) + 1 TwrFADmp(2) - Tower 2nd fore-aft mode structural damping ratio (%) + 1 TwrSSDmp(1) - Tower 1st side-to-side mode structural damping ratio (%) + 1 TwrSSDmp(2) - Tower 2nd side-to-side mode structural damping ratio (%) +---------------------- TOWER ADJUSTMUNT FACTORS -------------------------------- + 1 FAStTunr(1) - Tower fore-aft modal stiffness tuner, 1st mode (-) + 1 FAStTunr(2) - Tower fore-aft modal stiffness tuner, 2nd mode (-) + 1 SSStTunr(1) - Tower side-to-side stiffness tuner, 1st mode (-) + 1 SSStTunr(2) - Tower side-to-side stiffness tuner, 2nd mode (-) + 1 AdjTwMa - Factor to adjust tower mass density (-) + 1 AdjFASt - Factor to adjust tower fore-aft stiffness (-) + 1 AdjSSSt - Factor to adjust tower side-to-side stiffness (-) +---------------------- DISTRIBUTED TOWER PROPERTIES ---------------------------- + HtFract TMassDen TwFAStif TwSSStif + (-) (kg/m) (Nm^2) (Nm^2) +0.0000000E+00 5.5908700E+03 6.1434300E+11 6.1434300E+11 +1.0000000E-01 5.2324300E+03 5.3482100E+11 5.3482100E+11 +2.0000000E-01 4.8857600E+03 4.6326700E+11 4.6326700E+11 +3.0000000E-01 4.5508700E+03 3.9913100E+11 3.9913100E+11 +4.0000000E-01 4.2277500E+03 3.4188300E+11 3.4188300E+11 +5.0000000E-01 3.9164100E+03 2.9101100E+11 2.9101100E+11 +6.0000000E-01 3.6168300E+03 2.4602700E+11 2.4602700E+11 +7.0000000E-01 3.3290300E+03 2.0645700E+11 2.0645700E+11 +8.0000000E-01 3.0530100E+03 1.7185100E+11 1.7185100E+11 +9.0000000E-01 2.7887500E+03 1.4177600E+11 1.4177600E+11 +1.0000000E+00 2.5362700E+03 1.1582000E+11 1.1582000E+11 +---------------------- TOWER FORE-AFT MODE SHAPES ------------------------------ + 0.7004 TwFAM1Sh(2) - Mode 1, coefficient of x^2 term + 2.1963 TwFAM1Sh(3) - , coefficient of x^3 term + -5.6202 TwFAM1Sh(4) - , coefficient of x^4 term + 6.2275 TwFAM1Sh(5) - , coefficient of x^5 term + -2.504 TwFAM1Sh(6) - , coefficient of x^6 term + -70.5319 TwFAM2Sh(2) - Mode 2, coefficient of x^2 term + -63.7623 TwFAM2Sh(3) - , coefficient of x^3 term + 289.737 TwFAM2Sh(4) - , coefficient of x^4 term + -176.513 TwFAM2Sh(5) - , coefficient of x^5 term + 22.0706 TwFAM2Sh(6) - , coefficient of x^6 term +---------------------- TOWER SIDE-TO-SIDE MODE SHAPES -------------------------- + 1.385 TwSSM1Sh(2) - Mode 1, coefficient of x^2 term + -1.7684 TwSSM1Sh(3) - , coefficient of x^3 term + 3.0871 TwSSM1Sh(4) - , coefficient of x^4 term + -2.2395 TwSSM1Sh(5) - , coefficient of x^5 term + 0.5357 TwSSM1Sh(6) - , coefficient of x^6 term + -121.21 TwSSM2Sh(2) - Mode 2, coefficient of x^2 term + 184.415 TwSSM2Sh(3) - , coefficient of x^3 term + -224.904 TwSSM2Sh(4) - , coefficient of x^4 term + 298.536 TwSSM2Sh(5) - , coefficient of x^5 term + -135.838 TwSSM2Sh(6) - , coefficient of x^6 term + + diff --git a/examples/FAST.Farm_interface/inputs/FFFiles/NRELOffshrBsline5MW_Onshore_ServoDyn.T1_mod.dat b/examples/FAST.Farm_interface/inputs/FFFiles/NRELOffshrBsline5MW_Onshore_ServoDyn.T1_mod.dat new file mode 100644 index 00000000..3994ba11 --- /dev/null +++ b/examples/FAST.Farm_interface/inputs/FFFiles/NRELOffshrBsline5MW_Onshore_ServoDyn.T1_mod.dat @@ -0,0 +1,110 @@ +------- SERVODYN v1.05.* INPUT FILE -------------------------------------------- +NREL MW - Baseline Wind Turbine for Use in Offshore Analysis. Properties from Dutch Offshore Wind Energy Converter (DOWEC) 6MW Pre-Design (10046_009.pdf) and REpower 5M 5MW (5m_uk.pdf) +---------------------- SIMULATION CONTROL -------------------------------------- +False Echo - Echo input data to .ech (flag) +"default" DT - Communication interval for controllers (s) (or "default") +---------------------- PITCH CONTROL ------------------------------------------- +5 PCMode - Pitch control mode {0: none, 3: user-defined from routine PitchCntrl, 4: user-defined from Simulink/Labview, 5: user-defined from Bladed-style DLL} (switch) +0 TPCOn - Time to enable active pitch control (s) [unused when PCMode=0] +9999.9 TPitManS(1) - Time to start override pitch maneuver for blade 1 and end standard pitch control (s) +9999.9 TPitManS(2) - Time to start override pitch maneuver for blade 2 and end standard pitch control (s) +9999.9 TPitManS(3) - Time to start override pitch maneuver for blade 3 and end standard pitch control (s) [unused for 2 blades] +2 PitManRat(1) - Pitch rate at which override pitch maneuver heads toward final pitch angle for blade 1 (deg/s) +2 PitManRat(2) - Pitch rate at which override pitch maneuver heads toward final pitch angle for blade 2 (deg/s) +2 PitManRat(3) - Pitch rate at which override pitch maneuver heads toward final pitch angle for blade 3 (deg/s) [unused for 2 blades] +0 BlPitchF(1) - Blade 1 final pitch for pitch maneuvers (degrees) +0 BlPitchF(2) - Blade 2 final pitch for pitch maneuvers (degrees) +0 BlPitchF(3) - Blade 3 final pitch for pitch maneuvers (degrees) [unused for 2 blades] +---------------------- GENERATOR AND TORQUE CONTROL ---------------------------- +5 VSContrl - Variable-speed control mode {0: none, 1: simple VS, 3: user-defined from routine UserVSCont, 4: user-defined from Simulink/Labview, 5: user-defined from Bladed-style DLL} (switch) +2 GenModel - Generator model {1: simple, 2: Thevenin, 3: user-defined from routine UserGen} (switch) [used only when VSContrl=0] +94.4 GenEff - Generator efficiency [ignored by the Thevenin and user-defined generator models] (%) +True GenTiStr - Method to start the generator {T: timed using TimGenOn, F: generator speed using SpdGenOn} (flag) +True GenTiStp - Method to stop the generator {T: timed using TimGenOf, F: when generator power = 0} (flag) +9999.9 SpdGenOn - Generator speed to turn on the generator for a startup (HSS speed) (rpm) [used only when GenTiStr=False] +0 TimGenOn - Time to turn on the generator for a startup (s) [used only when GenTiStr=True] +9999.9 TimGenOf - Time to turn off the generator (s) [used only when GenTiStp=True] +---------------------- SIMPLE VARIABLE-SPEED TORQUE CONTROL -------------------- +9999.9 VS_RtGnSp - Rated generator speed for simple variable-speed generator control (HSS side) (rpm) [used only when VSContrl=1] +9999.9 VS_RtTq - Rated generator torque/constant generator torque in Region 3 for simple variable-speed generator control (HSS side) (N-m) [used only when VSContrl=1] +9999.9 VS_Rgn2K - Generator torque constant in Region 2 for simple variable-speed generator control (HSS side) (N-m/rpm^2) [used only when VSContrl=1] +9999.9 VS_SlPc - Rated generator slip percentage in Region 2 1/2 for simple variable-speed generator control (%) [used only when VSContrl=1] +---------------------- SIMPLE INDUCTION GENERATOR ------------------------------ +9999.9 SIG_SlPc - Rated generator slip percentage (%) [used only when VSContrl=0 and GenModel=1] +9999.9 SIG_SySp - Synchronous (zero-torque) generator speed (rpm) [used only when VSContrl=0 and GenModel=1] +9999.9 SIG_RtTq - Rated torque (N-m) [used only when VSContrl=0 and GenModel=1] +9999.9 SIG_PORt - Pull-out ratio (Tpullout/Trated) (-) [used only when VSContrl=0 and GenModel=1] +---------------------- THEVENIN-EQUIVALENT INDUCTION GENERATOR ----------------- +9999.9 TEC_Freq - Line frequency [50 or 60] (Hz) [used only when VSContrl=0 and GenModel=2] +9998 TEC_NPol - Number of poles [even integer > 0] (-) [used only when VSContrl=0 and GenModel=2] +9999.9 TEC_SRes - Stator resistance (ohms) [used only when VSContrl=0 and GenModel=2] +9999.9 TEC_RRes - Rotor resistance (ohms) [used only when VSContrl=0 and GenModel=2] +9999.9 TEC_VLL - Line-to-line RMS voltage (volts) [used only when VSContrl=0 and GenModel=2] +9999.9 TEC_SLR - Stator leakage reactance (ohms) [used only when VSContrl=0 and GenModel=2] +9999.9 TEC_RLR - Rotor leakage reactance (ohms) [used only when VSContrl=0 and GenModel=2] +9999.9 TEC_MR - Magnetizing reactance (ohms) [used only when VSContrl=0 and GenModel=2] +---------------------- HIGH-SPEED SHAFT BRAKE ---------------------------------- +0 HSSBrMode - HSS brake model {0: none, 1: simple, 3: user-defined from routine UserHSSBr, 4: user-defined from Simulink/Labview, 5: user-defined from Bladed-style DLL} (switch) +9999.9 THSSBrDp - Time to initiate deployment of the HSS brake (s) +0.6 HSSBrDT - Time for HSS-brake to reach full deployment once initiated (sec) [used only when HSSBrMode=1] +28116.2 HSSBrTqF - Fully deployed HSS-brake torque (N-m) +---------------------- NACELLE-YAW CONTROL ------------------------------------- +0 YCMode - Yaw control mode {0: none, 3: user-defined from routine UserYawCont, 4: user-defined from Simulink/Labview, 5: user-defined from Bladed-style DLL} (switch) +9999.9 TYCOn - Time to enable active yaw control (s) [unused when YCMode=0] +0 YawNeut - Neutral yaw position--yaw spring force is zero at this yaw (degrees) +9028320000.0 YawSpr - Nacelle-yaw spring constant (N-m/rad) +19160000.0 YawDamp - Nacelle-yaw damping constant (N-m/(rad/s)) +9999.9 TYawManS - Time to start override yaw maneuver and end standard yaw control (s) +2 YawManRat - Yaw maneuver rate (in absolute value) (deg/s) +0 NacYawF - Final yaw angle for override yaw maneuvers (degrees) +---------------------- AERODYNAMIC FLOW CONTROL -------------------------------- +0 AfCmode - Airfoil control mode {0: none, 1: cosine wave cycle, 4: user-defined from Simulink/Labview, 5: user-defined from Bladed-style DLL} (switch) +0 AfC_Mean - Mean level for cosine cycling or steady value (-) [used only with AfCmode==1] +0 AfC_Amp - Amplitude for for cosine cycling of flap signal (-) [used only with AfCmode==1] +0 AfC_Phase - Phase relative to the blade azimuth (0 is vertical) for for cosine cycling of flap signal (deg) [used only with AfCmode==1] +---------------------- STRUCTURAL CONTROL -------------------------------------- +0 NumBStC - Number of blade structural controllers (integer) +"unused" BStCfiles - Name of the files for blade structural controllers (quoted strings) [unused when NumBStC==0] +0 NumNStC - Number of nacelle structural controllers (integer) +"unused" NStCfiles - Name of the files for nacelle structural controllers (quoted strings) [unused when NumNStC==0] +0 NumTStC - Number of tower structural controllers (integer) +"unused" TStCfiles - Name of the files for tower structural controllers (quoted strings) [unused when NumTStC==0] +0 NumSStC - Number of substructure structural controllers (integer) +"unused" SStCfiles - Name of the files for substructure structural controllers (quoted strings) [unused when NumSStC==0] +---------------------- CABLE CONTROL ------------------------------------------- +0 CCmode - Cable control mode {0: none, 4: user-defined from Simulink/Labview, 5: user-defined from Bladed-style DLL} (switch) +---------------------- BLADED INTERFACE ---------------------------------------- [used only with Bladed Interface] +"libdiscon_WT1.so" DLL_FileName - Name/location of the dynamic library {.dll [Windows] or .so [Linux]} in the Bladed-DLL format (-) [used only with Bladed Interface] +"DISCON_WT1.IN" DLL_InFile - Name of input file sent to the DLL (-) [used only with Bladed Interface] +"DISCON" DLL_ProcName - Name of procedure in DLL to be called (-) [case sensitive; used only with DLL Interface] +"default" DLL_DT - Communication interval for dynamic library (s) (or "default") [used only with Bladed Interface] +False DLL_Ramp - Whether a linear ramp should be used between DLL_DT time steps [introduces time shift when true] (flag) [used only with Bladed Interface] +9999.9 BPCutoff - Cutoff frequency for low-pass filter on blade pitch from DLL (Hz) [used only with Bladed Interface] +0 NacYaw_North - Reference yaw angle of the nacelle when the upwind end points due North (deg) [used only with Bladed Interface] +0 Ptch_Cntrl - Record 28: Use individual pitch control {0: collective pitch; 1: individual pitch control} (switch) [used only with Bladed Interface] +0 Ptch_SetPnt - Record 5: Below-rated pitch angle set-point (deg) [used only with Bladed Interface] +0 Ptch_Min - Record 6: Minimum pitch angle (deg) [used only with Bladed Interface] +0 Ptch_Max - Record 7: Maximum pitch angle (deg) [used only with Bladed Interface] +0 PtchRate_Min - Record 8: Minimum pitch rate (most negative value allowed) (deg/s) [used only with Bladed Interface] +0 PtchRate_Max - Record 9: Maximum pitch rate (deg/s) [used only with Bladed Interface] +0 Gain_OM - Record 16: Optimal mode gain (Nm/(rad/s)^2) [used only with Bladed Interface] +0 GenSpd_MinOM - Record 17: Minimum generator speed (rpm) [used only with Bladed Interface] +0 GenSpd_MaxOM - Record 18: Optimal mode maximum speed (rpm) [used only with Bladed Interface] +0 GenSpd_Dem - Record 19: Demanded generator speed above rated (rpm) [used only with Bladed Interface] +0 GenTrq_Dem - Record 22: Demanded generator torque above rated (Nm) [used only with Bladed Interface] +0 GenPwr_Dem - Record 13: Demanded power (W) [used only with Bladed Interface] +---------------------- BLADED INTERFACE TORQUE-SPEED LOOK-UP TABLE ------------- +0 DLL_NumTrq - Record 26: No. of points in torque-speed look-up table {0 = none and use the optimal mode parameters; nonzero = ignore the optimal mode PARAMETERs by setting Record 16 to 0.0} (-) [used only with Bladed Interface] +GenSpd_TLU GenTrq_TLU +(rpm) (Nm) +---------------------- OUTPUT -------------------------------------------------- +False SumPrint - Print summary data to .sum (flag) (currently unused) +1 OutFile - Switch to determine where output will be placed: {1: in module output file only; 2: in glue code output file only; 3: both} (currently unused) +True TabDelim - Use tab delimiters in text tabular output file? (flag) (currently unused) +"ES10.3E2" OutFmt - Format used for text tabular output (except time). Resulting field should be 10 characters. (quoted string) (currently unused) +0 TStart - Time to begin tabular output (s) (currently unused) + OutList The next line(s) contains a list of output parameters. See OutListParameters.xlsx for a listing of available output channels, (-) +"GenPwr" - Electrical generator power and torque +"GenTq" - Electrical generator power and torque +END +--------------------------------------------------------------------------------------- \ No newline at end of file diff --git a/examples/FAST.Farm_interface/inputs/FFFiles/NRELOffshrBsline5MW_Onshore_ServoDyn.T2_mod.dat b/examples/FAST.Farm_interface/inputs/FFFiles/NRELOffshrBsline5MW_Onshore_ServoDyn.T2_mod.dat new file mode 100644 index 00000000..09bb573f --- /dev/null +++ b/examples/FAST.Farm_interface/inputs/FFFiles/NRELOffshrBsline5MW_Onshore_ServoDyn.T2_mod.dat @@ -0,0 +1,110 @@ +------- SERVODYN v1.05.* INPUT FILE -------------------------------------------- +NREL MW - Baseline Wind Turbine for Use in Offshore Analysis. Properties from Dutch Offshore Wind Energy Converter (DOWEC) 6MW Pre-Design (10046_009.pdf) and REpower 5M 5MW (5m_uk.pdf) +---------------------- SIMULATION CONTROL -------------------------------------- +False Echo - Echo input data to .ech (flag) +"default" DT - Communication interval for controllers (s) (or "default") +---------------------- PITCH CONTROL ------------------------------------------- +5 PCMode - Pitch control mode {0: none, 3: user-defined from routine PitchCntrl, 4: user-defined from Simulink/Labview, 5: user-defined from Bladed-style DLL} (switch) +0 TPCOn - Time to enable active pitch control (s) [unused when PCMode=0] +9999.9 TPitManS(1) - Time to start override pitch maneuver for blade 1 and end standard pitch control (s) +9999.9 TPitManS(2) - Time to start override pitch maneuver for blade 2 and end standard pitch control (s) +9999.9 TPitManS(3) - Time to start override pitch maneuver for blade 3 and end standard pitch control (s) [unused for 2 blades] +2 PitManRat(1) - Pitch rate at which override pitch maneuver heads toward final pitch angle for blade 1 (deg/s) +2 PitManRat(2) - Pitch rate at which override pitch maneuver heads toward final pitch angle for blade 2 (deg/s) +2 PitManRat(3) - Pitch rate at which override pitch maneuver heads toward final pitch angle for blade 3 (deg/s) [unused for 2 blades] +0 BlPitchF(1) - Blade 1 final pitch for pitch maneuvers (degrees) +0 BlPitchF(2) - Blade 2 final pitch for pitch maneuvers (degrees) +0 BlPitchF(3) - Blade 3 final pitch for pitch maneuvers (degrees) [unused for 2 blades] +---------------------- GENERATOR AND TORQUE CONTROL ---------------------------- +5 VSContrl - Variable-speed control mode {0: none, 1: simple VS, 3: user-defined from routine UserVSCont, 4: user-defined from Simulink/Labview, 5: user-defined from Bladed-style DLL} (switch) +2 GenModel - Generator model {1: simple, 2: Thevenin, 3: user-defined from routine UserGen} (switch) [used only when VSContrl=0] +94.4 GenEff - Generator efficiency [ignored by the Thevenin and user-defined generator models] (%) +True GenTiStr - Method to start the generator {T: timed using TimGenOn, F: generator speed using SpdGenOn} (flag) +True GenTiStp - Method to stop the generator {T: timed using TimGenOf, F: when generator power = 0} (flag) +9999.9 SpdGenOn - Generator speed to turn on the generator for a startup (HSS speed) (rpm) [used only when GenTiStr=False] +0 TimGenOn - Time to turn on the generator for a startup (s) [used only when GenTiStr=True] +9999.9 TimGenOf - Time to turn off the generator (s) [used only when GenTiStp=True] +---------------------- SIMPLE VARIABLE-SPEED TORQUE CONTROL -------------------- +9999.9 VS_RtGnSp - Rated generator speed for simple variable-speed generator control (HSS side) (rpm) [used only when VSContrl=1] +9999.9 VS_RtTq - Rated generator torque/constant generator torque in Region 3 for simple variable-speed generator control (HSS side) (N-m) [used only when VSContrl=1] +9999.9 VS_Rgn2K - Generator torque constant in Region 2 for simple variable-speed generator control (HSS side) (N-m/rpm^2) [used only when VSContrl=1] +9999.9 VS_SlPc - Rated generator slip percentage in Region 2 1/2 for simple variable-speed generator control (%) [used only when VSContrl=1] +---------------------- SIMPLE INDUCTION GENERATOR ------------------------------ +9999.9 SIG_SlPc - Rated generator slip percentage (%) [used only when VSContrl=0 and GenModel=1] +9999.9 SIG_SySp - Synchronous (zero-torque) generator speed (rpm) [used only when VSContrl=0 and GenModel=1] +9999.9 SIG_RtTq - Rated torque (N-m) [used only when VSContrl=0 and GenModel=1] +9999.9 SIG_PORt - Pull-out ratio (Tpullout/Trated) (-) [used only when VSContrl=0 and GenModel=1] +---------------------- THEVENIN-EQUIVALENT INDUCTION GENERATOR ----------------- +9999.9 TEC_Freq - Line frequency [50 or 60] (Hz) [used only when VSContrl=0 and GenModel=2] +9998 TEC_NPol - Number of poles [even integer > 0] (-) [used only when VSContrl=0 and GenModel=2] +9999.9 TEC_SRes - Stator resistance (ohms) [used only when VSContrl=0 and GenModel=2] +9999.9 TEC_RRes - Rotor resistance (ohms) [used only when VSContrl=0 and GenModel=2] +9999.9 TEC_VLL - Line-to-line RMS voltage (volts) [used only when VSContrl=0 and GenModel=2] +9999.9 TEC_SLR - Stator leakage reactance (ohms) [used only when VSContrl=0 and GenModel=2] +9999.9 TEC_RLR - Rotor leakage reactance (ohms) [used only when VSContrl=0 and GenModel=2] +9999.9 TEC_MR - Magnetizing reactance (ohms) [used only when VSContrl=0 and GenModel=2] +---------------------- HIGH-SPEED SHAFT BRAKE ---------------------------------- +0 HSSBrMode - HSS brake model {0: none, 1: simple, 3: user-defined from routine UserHSSBr, 4: user-defined from Simulink/Labview, 5: user-defined from Bladed-style DLL} (switch) +9999.9 THSSBrDp - Time to initiate deployment of the HSS brake (s) +0.6 HSSBrDT - Time for HSS-brake to reach full deployment once initiated (sec) [used only when HSSBrMode=1] +28116.2 HSSBrTqF - Fully deployed HSS-brake torque (N-m) +---------------------- NACELLE-YAW CONTROL ------------------------------------- +0 YCMode - Yaw control mode {0: none, 3: user-defined from routine UserYawCont, 4: user-defined from Simulink/Labview, 5: user-defined from Bladed-style DLL} (switch) +9999.9 TYCOn - Time to enable active yaw control (s) [unused when YCMode=0] +0 YawNeut - Neutral yaw position--yaw spring force is zero at this yaw (degrees) +9028320000.0 YawSpr - Nacelle-yaw spring constant (N-m/rad) +19160000.0 YawDamp - Nacelle-yaw damping constant (N-m/(rad/s)) +9999.9 TYawManS - Time to start override yaw maneuver and end standard yaw control (s) +2 YawManRat - Yaw maneuver rate (in absolute value) (deg/s) +0 NacYawF - Final yaw angle for override yaw maneuvers (degrees) +---------------------- AERODYNAMIC FLOW CONTROL -------------------------------- +0 AfCmode - Airfoil control mode {0: none, 1: cosine wave cycle, 4: user-defined from Simulink/Labview, 5: user-defined from Bladed-style DLL} (switch) +0 AfC_Mean - Mean level for cosine cycling or steady value (-) [used only with AfCmode==1] +0 AfC_Amp - Amplitude for for cosine cycling of flap signal (-) [used only with AfCmode==1] +0 AfC_Phase - Phase relative to the blade azimuth (0 is vertical) for for cosine cycling of flap signal (deg) [used only with AfCmode==1] +---------------------- STRUCTURAL CONTROL -------------------------------------- +0 NumBStC - Number of blade structural controllers (integer) +"unused" BStCfiles - Name of the files for blade structural controllers (quoted strings) [unused when NumBStC==0] +0 NumNStC - Number of nacelle structural controllers (integer) +"unused" NStCfiles - Name of the files for nacelle structural controllers (quoted strings) [unused when NumNStC==0] +0 NumTStC - Number of tower structural controllers (integer) +"unused" TStCfiles - Name of the files for tower structural controllers (quoted strings) [unused when NumTStC==0] +0 NumSStC - Number of substructure structural controllers (integer) +"unused" SStCfiles - Name of the files for substructure structural controllers (quoted strings) [unused when NumSStC==0] +---------------------- CABLE CONTROL ------------------------------------------- +0 CCmode - Cable control mode {0: none, 4: user-defined from Simulink/Labview, 5: user-defined from Bladed-style DLL} (switch) +---------------------- BLADED INTERFACE ---------------------------------------- [used only with Bladed Interface] +"libdiscon_WT2.so" DLL_FileName - Name/location of the dynamic library {.dll [Windows] or .so [Linux]} in the Bladed-DLL format (-) [used only with Bladed Interface] +"DISCON_WT2.IN" DLL_InFile - Name of input file sent to the DLL (-) [used only with Bladed Interface] +"DISCON" DLL_ProcName - Name of procedure in DLL to be called (-) [case sensitive; used only with DLL Interface] +"default" DLL_DT - Communication interval for dynamic library (s) (or "default") [used only with Bladed Interface] +False DLL_Ramp - Whether a linear ramp should be used between DLL_DT time steps [introduces time shift when true] (flag) [used only with Bladed Interface] +9999.9 BPCutoff - Cutoff frequency for low-pass filter on blade pitch from DLL (Hz) [used only with Bladed Interface] +0 NacYaw_North - Reference yaw angle of the nacelle when the upwind end points due North (deg) [used only with Bladed Interface] +0 Ptch_Cntrl - Record 28: Use individual pitch control {0: collective pitch; 1: individual pitch control} (switch) [used only with Bladed Interface] +0 Ptch_SetPnt - Record 5: Below-rated pitch angle set-point (deg) [used only with Bladed Interface] +0 Ptch_Min - Record 6: Minimum pitch angle (deg) [used only with Bladed Interface] +0 Ptch_Max - Record 7: Maximum pitch angle (deg) [used only with Bladed Interface] +0 PtchRate_Min - Record 8: Minimum pitch rate (most negative value allowed) (deg/s) [used only with Bladed Interface] +0 PtchRate_Max - Record 9: Maximum pitch rate (deg/s) [used only with Bladed Interface] +0 Gain_OM - Record 16: Optimal mode gain (Nm/(rad/s)^2) [used only with Bladed Interface] +0 GenSpd_MinOM - Record 17: Minimum generator speed (rpm) [used only with Bladed Interface] +0 GenSpd_MaxOM - Record 18: Optimal mode maximum speed (rpm) [used only with Bladed Interface] +0 GenSpd_Dem - Record 19: Demanded generator speed above rated (rpm) [used only with Bladed Interface] +0 GenTrq_Dem - Record 22: Demanded generator torque above rated (Nm) [used only with Bladed Interface] +0 GenPwr_Dem - Record 13: Demanded power (W) [used only with Bladed Interface] +---------------------- BLADED INTERFACE TORQUE-SPEED LOOK-UP TABLE ------------- +0 DLL_NumTrq - Record 26: No. of points in torque-speed look-up table {0 = none and use the optimal mode parameters; nonzero = ignore the optimal mode PARAMETERs by setting Record 16 to 0.0} (-) [used only with Bladed Interface] +GenSpd_TLU GenTrq_TLU +(rpm) (Nm) +---------------------- OUTPUT -------------------------------------------------- +False SumPrint - Print summary data to .sum (flag) (currently unused) +1 OutFile - Switch to determine where output will be placed: {1: in module output file only; 2: in glue code output file only; 3: both} (currently unused) +True TabDelim - Use tab delimiters in text tabular output file? (flag) (currently unused) +"ES10.3E2" OutFmt - Format used for text tabular output (except time). Resulting field should be 10 characters. (quoted string) (currently unused) +0 TStart - Time to begin tabular output (s) (currently unused) + OutList The next line(s) contains a list of output parameters. See OutListParameters.xlsx for a listing of available output channels, (-) +"GenPwr" - Electrical generator power and torque +"GenTq" - Electrical generator power and torque +END +--------------------------------------------------------------------------------------- \ No newline at end of file diff --git a/examples/FAST.Farm_interface/inputs/FFFiles/NRELOffshrBsline5MW_Onshore_ServoDyn.T3_mod.dat b/examples/FAST.Farm_interface/inputs/FFFiles/NRELOffshrBsline5MW_Onshore_ServoDyn.T3_mod.dat new file mode 100644 index 00000000..6d9d87cd --- /dev/null +++ b/examples/FAST.Farm_interface/inputs/FFFiles/NRELOffshrBsline5MW_Onshore_ServoDyn.T3_mod.dat @@ -0,0 +1,110 @@ +------- SERVODYN v1.05.* INPUT FILE -------------------------------------------- +NREL MW - Baseline Wind Turbine for Use in Offshore Analysis. Properties from Dutch Offshore Wind Energy Converter (DOWEC) 6MW Pre-Design (10046_009.pdf) and REpower 5M 5MW (5m_uk.pdf) +---------------------- SIMULATION CONTROL -------------------------------------- +False Echo - Echo input data to .ech (flag) +"default" DT - Communication interval for controllers (s) (or "default") +---------------------- PITCH CONTROL ------------------------------------------- +5 PCMode - Pitch control mode {0: none, 3: user-defined from routine PitchCntrl, 4: user-defined from Simulink/Labview, 5: user-defined from Bladed-style DLL} (switch) +0 TPCOn - Time to enable active pitch control (s) [unused when PCMode=0] +9999.9 TPitManS(1) - Time to start override pitch maneuver for blade 1 and end standard pitch control (s) +9999.9 TPitManS(2) - Time to start override pitch maneuver for blade 2 and end standard pitch control (s) +9999.9 TPitManS(3) - Time to start override pitch maneuver for blade 3 and end standard pitch control (s) [unused for 2 blades] +2 PitManRat(1) - Pitch rate at which override pitch maneuver heads toward final pitch angle for blade 1 (deg/s) +2 PitManRat(2) - Pitch rate at which override pitch maneuver heads toward final pitch angle for blade 2 (deg/s) +2 PitManRat(3) - Pitch rate at which override pitch maneuver heads toward final pitch angle for blade 3 (deg/s) [unused for 2 blades] +0 BlPitchF(1) - Blade 1 final pitch for pitch maneuvers (degrees) +0 BlPitchF(2) - Blade 2 final pitch for pitch maneuvers (degrees) +0 BlPitchF(3) - Blade 3 final pitch for pitch maneuvers (degrees) [unused for 2 blades] +---------------------- GENERATOR AND TORQUE CONTROL ---------------------------- +5 VSContrl - Variable-speed control mode {0: none, 1: simple VS, 3: user-defined from routine UserVSCont, 4: user-defined from Simulink/Labview, 5: user-defined from Bladed-style DLL} (switch) +2 GenModel - Generator model {1: simple, 2: Thevenin, 3: user-defined from routine UserGen} (switch) [used only when VSContrl=0] +94.4 GenEff - Generator efficiency [ignored by the Thevenin and user-defined generator models] (%) +True GenTiStr - Method to start the generator {T: timed using TimGenOn, F: generator speed using SpdGenOn} (flag) +True GenTiStp - Method to stop the generator {T: timed using TimGenOf, F: when generator power = 0} (flag) +9999.9 SpdGenOn - Generator speed to turn on the generator for a startup (HSS speed) (rpm) [used only when GenTiStr=False] +0 TimGenOn - Time to turn on the generator for a startup (s) [used only when GenTiStr=True] +9999.9 TimGenOf - Time to turn off the generator (s) [used only when GenTiStp=True] +---------------------- SIMPLE VARIABLE-SPEED TORQUE CONTROL -------------------- +9999.9 VS_RtGnSp - Rated generator speed for simple variable-speed generator control (HSS side) (rpm) [used only when VSContrl=1] +9999.9 VS_RtTq - Rated generator torque/constant generator torque in Region 3 for simple variable-speed generator control (HSS side) (N-m) [used only when VSContrl=1] +9999.9 VS_Rgn2K - Generator torque constant in Region 2 for simple variable-speed generator control (HSS side) (N-m/rpm^2) [used only when VSContrl=1] +9999.9 VS_SlPc - Rated generator slip percentage in Region 2 1/2 for simple variable-speed generator control (%) [used only when VSContrl=1] +---------------------- SIMPLE INDUCTION GENERATOR ------------------------------ +9999.9 SIG_SlPc - Rated generator slip percentage (%) [used only when VSContrl=0 and GenModel=1] +9999.9 SIG_SySp - Synchronous (zero-torque) generator speed (rpm) [used only when VSContrl=0 and GenModel=1] +9999.9 SIG_RtTq - Rated torque (N-m) [used only when VSContrl=0 and GenModel=1] +9999.9 SIG_PORt - Pull-out ratio (Tpullout/Trated) (-) [used only when VSContrl=0 and GenModel=1] +---------------------- THEVENIN-EQUIVALENT INDUCTION GENERATOR ----------------- +9999.9 TEC_Freq - Line frequency [50 or 60] (Hz) [used only when VSContrl=0 and GenModel=2] +9998 TEC_NPol - Number of poles [even integer > 0] (-) [used only when VSContrl=0 and GenModel=2] +9999.9 TEC_SRes - Stator resistance (ohms) [used only when VSContrl=0 and GenModel=2] +9999.9 TEC_RRes - Rotor resistance (ohms) [used only when VSContrl=0 and GenModel=2] +9999.9 TEC_VLL - Line-to-line RMS voltage (volts) [used only when VSContrl=0 and GenModel=2] +9999.9 TEC_SLR - Stator leakage reactance (ohms) [used only when VSContrl=0 and GenModel=2] +9999.9 TEC_RLR - Rotor leakage reactance (ohms) [used only when VSContrl=0 and GenModel=2] +9999.9 TEC_MR - Magnetizing reactance (ohms) [used only when VSContrl=0 and GenModel=2] +---------------------- HIGH-SPEED SHAFT BRAKE ---------------------------------- +0 HSSBrMode - HSS brake model {0: none, 1: simple, 3: user-defined from routine UserHSSBr, 4: user-defined from Simulink/Labview, 5: user-defined from Bladed-style DLL} (switch) +9999.9 THSSBrDp - Time to initiate deployment of the HSS brake (s) +0.6 HSSBrDT - Time for HSS-brake to reach full deployment once initiated (sec) [used only when HSSBrMode=1] +28116.2 HSSBrTqF - Fully deployed HSS-brake torque (N-m) +---------------------- NACELLE-YAW CONTROL ------------------------------------- +0 YCMode - Yaw control mode {0: none, 3: user-defined from routine UserYawCont, 4: user-defined from Simulink/Labview, 5: user-defined from Bladed-style DLL} (switch) +9999.9 TYCOn - Time to enable active yaw control (s) [unused when YCMode=0] +0 YawNeut - Neutral yaw position--yaw spring force is zero at this yaw (degrees) +9028320000.0 YawSpr - Nacelle-yaw spring constant (N-m/rad) +19160000.0 YawDamp - Nacelle-yaw damping constant (N-m/(rad/s)) +9999.9 TYawManS - Time to start override yaw maneuver and end standard yaw control (s) +2 YawManRat - Yaw maneuver rate (in absolute value) (deg/s) +0 NacYawF - Final yaw angle for override yaw maneuvers (degrees) +---------------------- AERODYNAMIC FLOW CONTROL -------------------------------- +0 AfCmode - Airfoil control mode {0: none, 1: cosine wave cycle, 4: user-defined from Simulink/Labview, 5: user-defined from Bladed-style DLL} (switch) +0 AfC_Mean - Mean level for cosine cycling or steady value (-) [used only with AfCmode==1] +0 AfC_Amp - Amplitude for for cosine cycling of flap signal (-) [used only with AfCmode==1] +0 AfC_Phase - Phase relative to the blade azimuth (0 is vertical) for for cosine cycling of flap signal (deg) [used only with AfCmode==1] +---------------------- STRUCTURAL CONTROL -------------------------------------- +0 NumBStC - Number of blade structural controllers (integer) +"unused" BStCfiles - Name of the files for blade structural controllers (quoted strings) [unused when NumBStC==0] +0 NumNStC - Number of nacelle structural controllers (integer) +"unused" NStCfiles - Name of the files for nacelle structural controllers (quoted strings) [unused when NumNStC==0] +0 NumTStC - Number of tower structural controllers (integer) +"unused" TStCfiles - Name of the files for tower structural controllers (quoted strings) [unused when NumTStC==0] +0 NumSStC - Number of substructure structural controllers (integer) +"unused" SStCfiles - Name of the files for substructure structural controllers (quoted strings) [unused when NumSStC==0] +---------------------- CABLE CONTROL ------------------------------------------- +0 CCmode - Cable control mode {0: none, 4: user-defined from Simulink/Labview, 5: user-defined from Bladed-style DLL} (switch) +---------------------- BLADED INTERFACE ---------------------------------------- [used only with Bladed Interface] +"libdiscon_WT3.so" DLL_FileName - Name/location of the dynamic library {.dll [Windows] or .so [Linux]} in the Bladed-DLL format (-) [used only with Bladed Interface] +"DISCON_WT3.IN" DLL_InFile - Name of input file sent to the DLL (-) [used only with Bladed Interface] +"DISCON" DLL_ProcName - Name of procedure in DLL to be called (-) [case sensitive; used only with DLL Interface] +"default" DLL_DT - Communication interval for dynamic library (s) (or "default") [used only with Bladed Interface] +False DLL_Ramp - Whether a linear ramp should be used between DLL_DT time steps [introduces time shift when true] (flag) [used only with Bladed Interface] +9999.9 BPCutoff - Cutoff frequency for low-pass filter on blade pitch from DLL (Hz) [used only with Bladed Interface] +0 NacYaw_North - Reference yaw angle of the nacelle when the upwind end points due North (deg) [used only with Bladed Interface] +0 Ptch_Cntrl - Record 28: Use individual pitch control {0: collective pitch; 1: individual pitch control} (switch) [used only with Bladed Interface] +0 Ptch_SetPnt - Record 5: Below-rated pitch angle set-point (deg) [used only with Bladed Interface] +0 Ptch_Min - Record 6: Minimum pitch angle (deg) [used only with Bladed Interface] +0 Ptch_Max - Record 7: Maximum pitch angle (deg) [used only with Bladed Interface] +0 PtchRate_Min - Record 8: Minimum pitch rate (most negative value allowed) (deg/s) [used only with Bladed Interface] +0 PtchRate_Max - Record 9: Maximum pitch rate (deg/s) [used only with Bladed Interface] +0 Gain_OM - Record 16: Optimal mode gain (Nm/(rad/s)^2) [used only with Bladed Interface] +0 GenSpd_MinOM - Record 17: Minimum generator speed (rpm) [used only with Bladed Interface] +0 GenSpd_MaxOM - Record 18: Optimal mode maximum speed (rpm) [used only with Bladed Interface] +0 GenSpd_Dem - Record 19: Demanded generator speed above rated (rpm) [used only with Bladed Interface] +0 GenTrq_Dem - Record 22: Demanded generator torque above rated (Nm) [used only with Bladed Interface] +0 GenPwr_Dem - Record 13: Demanded power (W) [used only with Bladed Interface] +---------------------- BLADED INTERFACE TORQUE-SPEED LOOK-UP TABLE ------------- +0 DLL_NumTrq - Record 26: No. of points in torque-speed look-up table {0 = none and use the optimal mode parameters; nonzero = ignore the optimal mode PARAMETERs by setting Record 16 to 0.0} (-) [used only with Bladed Interface] +GenSpd_TLU GenTrq_TLU +(rpm) (Nm) +---------------------- OUTPUT -------------------------------------------------- +False SumPrint - Print summary data to .sum (flag) (currently unused) +1 OutFile - Switch to determine where output will be placed: {1: in module output file only; 2: in glue code output file only; 3: both} (currently unused) +True TabDelim - Use tab delimiters in text tabular output file? (flag) (currently unused) +"ES10.3E2" OutFmt - Format used for text tabular output (except time). Resulting field should be 10 characters. (quoted string) (currently unused) +0 TStart - Time to begin tabular output (s) (currently unused) + OutList The next line(s) contains a list of output parameters. See OutListParameters.xlsx for a listing of available output channels, (-) +"GenPwr" - Electrical generator power and torque +"GenTq" - Electrical generator power and torque +END +--------------------------------------------------------------------------------------- \ No newline at end of file diff --git a/examples/FAST.Farm_interface/inputs/FFFiles/TurbSim/HighT1.bts b/examples/FAST.Farm_interface/inputs/FFFiles/TurbSim/HighT1.bts new file mode 100644 index 00000000..521d2ee2 Binary files /dev/null and b/examples/FAST.Farm_interface/inputs/FFFiles/TurbSim/HighT1.bts differ diff --git a/examples/FAST.Farm_interface/inputs/FFFiles/TurbSim/HighT1.inp b/examples/FAST.Farm_interface/inputs/FFFiles/TurbSim/HighT1.inp new file mode 100644 index 00000000..ba4fdd7e --- /dev/null +++ b/examples/FAST.Farm_interface/inputs/FFFiles/TurbSim/HighT1.inp @@ -0,0 +1,74 @@ +--------TurbSim v2.00.* Input File------------------------ +for Certification - Test #1 (Kaimal Spectrum, formatted FF files). +---------Runtime Options----------------------------------- +False Echo - Echo input data to .ech (flag) +-281629 RandSeed1 - First random seed (-2147483648 to 2147483647) +RanLux RandSeed2 - Second random seed (-2147483648 to 2147483647) for intrinsic pRNG, or an alternative pRNG: "RanLux" or "RNSNLW" +False WrBHHTP - Output hub-height turbulence parameters in binary form? (Generates RootName.bin) +False WrFHHTP - Output hub-height turbulence parameters in formatted form? (Generates RootName.dat) +False WrADHH - Output hub-height time-series data in AeroDyn form? (Generates RootName.hh) +True WrADFF - Output full-field time-series data in TurbSim/AeroDyn form? (Generates RootName.bts) +False WrBLFF - Output full-field time-series data in BLADED/AeroDyn form? (Generates RootName.wnd) +False WrADTWR - Output tower time-series data? (Generates RootName.twr) +False WrFMTFF - Output full-field time-series data in formatted (readable) form? (Generates RootName.u, RootName.v, RootName.w) +False WrACT - Output coherent turbulence time steps in AeroDyn form? (Generates RootName.cts) +True Clockwise - Clockwise rotation looking downwind? (used only for full-field binary files - not necessary for AeroDyn) +0 ScaleIEC - Scale IEC turbulence models to exact target standard deviation? [0=no additional scaling; 1=use hub scale uniformly; 2=use individual scales] + +--------Turbine/Model Specifications----------------------- +37 NumGrid_Z - Vertical grid-point matrix dimension +35 NumGrid_Y - Horizontal grid-point matrix dimension +0.25 TimeStep - Time step [seconds] +600.0 AnalysisTime - Length of analysis time series [seconds] (program will add time if necessary: AnalysisTime = MAX(AnalysisTime, UsableTime+GridWidth/MeanHHWS) ) +"ALL" UsableTime - Usable length of output time series [seconds] (program will add GridWidth/MeanHHWS seconds unless UsableTime is "ALL") +89.35 HubHt - Hub height [m] (should be > 0.5*GridHeight) +167.4 GridHeight - Grid height [m] +158.1 GridWidth - Grid width [m] (should be >= 2*(RotorRadius+ShaftLength)) +0 VFlowAng - Vertical mean flow (uptilt) angle [degrees] +0 HFlowAng - Horizontal mean flow (skew) angle [degrees] + +--------Meteorological Boundary Conditions------------------- +"TIMESR" TurbModel - Turbulence model ("IECKAI","IECVKM","GP_LLJ","NWTCUP","SMOOTH","WF_UPW","WF_07D","WF_14D","TIDAL","API","USRINP","TIMESR", or "NONE") +"USRTimeSeries_T1.txt" UserFile - Name of the file that contains inputs for user-defined spectra or time series inputs (used only for "IECKAI" and "TIMESR" models) +1 IECstandard - Number of IEC 61400-x standard (x=1,2, or 3 with optional 61400-1 edition number (i.e. "1-Ed2") ) +"8.000 " IECturbc - IEC turbulence characteristic ("A", "B", "C" or the turbulence intensity in percent) ("KHTEST" option with NWTCUP model, not used for other models) +"NTM" IEC_WindType - IEC turbulence type ("NTM"=normal, "xETM"=extreme turbulence, "xEWM1"=extreme 1-year wind, "xEWM50"=extreme 50-year wind, where x=wind turbine class 1, 2, or 3) +"default" ETMc - IEC Extreme Turbulence Model "c" parameter [m/s] +"PL" WindProfileType - Velocity profile type ("LOG";"PL"=power law;"JET";"H2L"=Log law for TIDAL model;"API";"PL";"TS";"IEC"=PL on rotor disk, LOG elsewhere; or "default") +"unused" ProfileFile - Name of the file that contains input profiles for WindProfileType="USR" and/or TurbModel="USRVKM" [-] +90 RefHt - Height of the reference velocity (URef) [m] +8.0 URef - Mean (total) velocity at the reference height [m/s] (or "default" for JET velocity profile) [must be 1-hr mean for API model; otherwise is the mean over AnalysisTime seconds] +350 ZJetMax - Jet height [m] (used only for JET velocity profile, valid 70-490 m) +0.0 PLExp - Power law exponent [-] (or "default") +"default" Z0 - Surface roughness length [m] (or "default") + +--------Non-IEC Meteorological Boundary Conditions------------ +"default" Latitude - Site latitude [degrees] (or "default") +0.05 RICH_NO - Gradient Richardson number [-] +"default" UStar - Friction or shear velocity [m/s] (or "default") +"default" ZI - Mixing layer depth [m] (or "default") +"default" PC_UW - Hub mean u'w' Reynolds stress [m^2/s^2] (or "default" or "none") +"default" PC_UV - Hub mean u'v' Reynolds stress [m^2/s^2] (or "default" or "none") +"default" PC_VW - Hub mean v'w' Reynolds stress [m^2/s^2] (or "default" or "none") + +--------Spatial Coherence Parameters---------------------------- +"IEC" SCMod1 - u-component coherence model ("GENERAL","IEC","API","NONE", or "default") +"IEC" SCMod2 - v-component coherence model ("GENERAL","IEC","NONE", or "default") +"IEC" SCMod3 - w-component coherence model ("GENERAL","IEC","NONE", or "default") +"12 0.00035273" InCDec1 - u-component coherence parameters for general or IEC models [-, m^-1] (e.g. "10.0 0.3e-3" in quotes) (or "default") +"12 0.00035273" InCDec2 - v-component coherence parameters for general or IEC models [-, m^-1] (e.g. "10.0 0.3e-3" in quotes) (or "default") +"12 0.00035273" InCDec3 - w-component coherence parameters for general or IEC models [-, m^-1] (e.g. "10.0 0.3e-3" in quotes) (or "default") +"0.0" CohExp - Coherence exponent for general model [-] (or "default") + +--------Coherent Turbulence Scaling Parameters------------------- +".\EventData" CTEventPath - Name of the path where event data files are located +"random" CTEventFile - Type of event files ("LES", "DNS", or "RANDOM") +True Randomize - Randomize the disturbance scale and locations? (true/false) +1 DistScl - Disturbance scale [-] (ratio of event dataset height to rotor disk). (Ignored when Randomize = true.) +0.5 CTLy - Fractional location of tower centerline from right [-] (looking downwind) to left side of the dataset. (Ignored when Randomize = true.) +0.5 CTLz - Fractional location of hub height from the bottom of the dataset. [-] (Ignored when Randomize = true.) +30 CTStartTime - Minimum start time for coherent structures in RootName.cts [seconds] + +==================================================== +! NOTE: Do not add or remove any lines in this file! +==================================================== \ No newline at end of file diff --git a/examples/FAST.Farm_interface/inputs/FFFiles/TurbSim/HighT1.sum b/examples/FAST.Farm_interface/inputs/FFFiles/TurbSim/HighT1.sum new file mode 100644 index 00000000..89878aef --- /dev/null +++ b/examples/FAST.Farm_interface/inputs/FFFiles/TurbSim/HighT1.sum @@ -0,0 +1,331 @@ + +This summary file was generated by TurbSim (from OpenFAST-v3.5.3) on 20-Jun-2024 at 17:22:13. + + +Runtime Options: + + -281629 Random seed #1 + RANLUX Type of random number generator + F Output binary HH turbulence parameters? + F Output formatted turbulence parameters? + F Output AeroDyn HH files? + T Output AeroDyn FF files? + F Output BLADED FF files? + F Output tower data? + F Output HAWC FF files? + F Output formatted FF files? + T Output coherent turbulence time step file? + 0 - NONE IEC turbulence models scaled to exact specified standard deviation + + +Turbine/Model Specifications: + + 37 Vertical grid-point matrix dimension + 35 Horizontal grid-point matrix dimension + 0.250 Time step [seconds] + 600.000 Analysis time [seconds] + 600.000 Usable output time [seconds] + 89.350 Hub height [m] + 167.400 Grid height [m] + 158.100 Grid width [m] + 0.000 Vertical flow angle [degrees] + 0.000 Horizontal flow angle [degrees] + + +Meteorological Boundary Conditions: + + TIMESR User-input time series spectral model + N/A IEC standard + N/A IEC turbulence characteristic + N/A IEC turbulence type + N/A IEC Extreme Turbulence Model (ETM) "c" parameter [m/s] + PL Wind profile type + 90.000 Reference height [m] + 8.000 Reference wind speed [m/s] + N/A Jet height [m] + 0.000 Power law exponent + 0.030 Surface roughness length [m] + + +Non-IEC Meteorological Boundary Conditions: + + 45.000 Site latitude [degrees] + 0.050 Gradient Richardson number + 0.384 Friction or shear velocity [m/s] + N/A Mixing layer depth [m] + N/A Mean hub u'w' Reynolds stress + N/A Mean hub u'v' Reynolds stress + N/A Mean hub v'w' Reynolds stress + + +Spatial Coherence Models: + + IEC u-component coherence model + IEC v-component coherence model + IEC w-component coherence model +( 12.000, 0.353E-03) u-component coherence parameters +( 12.000, 0.353E-03) v-component coherence parameters +( 12.000, 0.353E-03) w-component coherence parameters + N/A Coherence exponent + + +Coherent Turbulence Scaling Parameters: + +.\EventData + Name of the path containing the coherent turbulence data files + dns Type of coherent turbulence data files + 1.000 Disturbance scale (ratio of wave height to rotor diameter) + 0.500 Fractional location of tower centerline from right + 0.500 Fractional location of hub height from the bottom of the dataset + 30.000 Minimum start time for coherent structures [seconds] + + +Profiles from User-Defined Time-Series Input: + + Height Wind Speed Horizontal Angle Vertical Angle + (m) (m/s) (deg) (deg) + ------ ---------- ---------------- -------------- + 94.00 8.00 0.00 0.00 + + +You have requested that the following file(s) be generated: + + ../FFSim/Cond00_v08.0_PL0.0_TI8/Case0_wdirp00/Seed_0/TurbSim/HighT1.bts (AeroDyn/TurbSim full-field wind file) + + +Turbulence Simulation Scaling Parameter Summary: + + Turbulence model used = User-input time series + Gradient Richardson number = 0.050 + Monin-Obukhov (M-O) z/L parameter = 0.067 + Monin-Obukhov (M-O) length scale = 1340.250 m + Mean wind speed at hub height = 8.000 m/s + + Wind profile type = Power law + Power law exponent = 0.000 + Mean shear across rotor disk = 0.000 (m/s)/m + Assumed rotor diameter = 158.100 m + Surface roughness length = 0.030 m + + Nyquist frequency of turbulent wind field = 2.000 Hz + + Number of time steps in the FFT = 2400 + Number of time steps output = 2400 + Number of points simulated = 1295 + + +Mean Flow Angles: + + Vertical = 0.0 degrees + Horizontal = 0.0 degrees + +Mean Wind Speed Profile: + + Height Wind Speed Horizontal Angle Vertical Angle U-comp (X) V-comp (Y) W-comp (Z) + (m) (m/s) (degrees) (degrees) (m/s) (m/s) (m/s) + ------ ---------- ---------------- -------------- ---------- ---------- ---------- + 168.4 8.00 0.00 0.00 8.00 0.00 0.00 + 163.7 8.00 0.00 0.00 8.00 0.00 0.00 + 159.1 8.00 0.00 0.00 8.00 0.00 0.00 + 154.4 8.00 0.00 0.00 8.00 0.00 0.00 + 149.8 8.00 0.00 0.00 8.00 0.00 0.00 + 145.1 8.00 0.00 0.00 8.00 0.00 0.00 + 140.5 8.00 0.00 0.00 8.00 0.00 0.00 + 135.8 8.00 0.00 0.00 8.00 0.00 0.00 + 131.2 8.00 0.00 0.00 8.00 0.00 0.00 + 126.5 8.00 0.00 0.00 8.00 0.00 0.00 + 121.9 8.00 0.00 0.00 8.00 0.00 0.00 + 117.2 8.00 0.00 0.00 8.00 0.00 0.00 + 112.6 8.00 0.00 0.00 8.00 0.00 0.00 + 107.9 8.00 0.00 0.00 8.00 0.00 0.00 + 103.3 8.00 0.00 0.00 8.00 0.00 0.00 + 98.6 8.00 0.00 0.00 8.00 0.00 0.00 + 94.0 8.00 0.00 0.00 8.00 0.00 0.00 + 89.3 8.00 0.00 0.00 8.00 0.00 0.00 + 84.7 8.00 0.00 0.00 8.00 0.00 0.00 + 80.0 8.00 0.00 0.00 8.00 0.00 0.00 + 75.4 8.00 0.00 0.00 8.00 0.00 0.00 + 70.7 8.00 0.00 0.00 8.00 0.00 0.00 + 66.1 8.00 0.00 0.00 8.00 0.00 0.00 + 61.4 8.00 0.00 0.00 8.00 0.00 0.00 + 56.8 8.00 0.00 0.00 8.00 0.00 0.00 + 52.1 8.00 0.00 0.00 8.00 0.00 0.00 + 47.5 8.00 0.00 0.00 8.00 0.00 0.00 + 42.8 8.00 0.00 0.00 8.00 0.00 0.00 + 38.2 8.00 0.00 0.00 8.00 0.00 0.00 + 33.5 8.00 0.00 0.00 8.00 0.00 0.00 + 28.9 8.00 0.00 0.00 8.00 0.00 0.00 + 24.2 8.00 0.00 0.00 8.00 0.00 0.00 + 19.6 8.00 0.00 0.00 8.00 0.00 0.00 + 14.9 8.00 0.00 0.00 8.00 0.00 0.00 + 10.3 8.00 0.00 0.00 8.00 0.00 0.00 + 5.6 8.00 0.00 0.00 8.00 0.00 0.00 + 1.0 8.00 0.00 0.00 8.00 0.00 0.00 + + +Harvested Random Seeds after Generation of the Random Numbers: + + 43317750 K 1 + 0 K 2 + + +Hub-Height Simulated Turbulence Statistical Summary: + + Type of Wind Min (m/s) Mean (m/s) Max (m/s) Sigma (m/s) TI (%) + ---------------- --------- ---------- --------- ----------- ------ + Longitudinal (u) 6.53 8.00 9.31 0.525 6.566 + Lateral (v) -1.34 0.00 1.25 0.518 6.478 + Vertical (w) -0.97 0.00 1.01 0.299 3.741 + U component 6.53 8.00 9.31 0.525 6.566 + V component -1.34 0.00 1.25 0.518 6.478 + W component -0.97 0.00 1.01 0.299 3.741 + Horizontal (U&V) 6.54 8.02 9.31 0.525 6.546 + Total 6.55 8.02 9.32 0.524 6.531 + + Min Reynolds Mean Reynolds Max Reynolds Correlation + Product Stress (m/s)^2 Stress (m/s)^2 Stress (m/s)^2 Coefficient + ---------------- -------------- -------------- -------------- ----------- + u'w' -0.837 0.012 0.866 0.073 + u'v' -1.249 -0.029 1.598 -0.108 + v'w' -0.798 0.006 0.995 0.040 + + + Friction Velocity (Ustar) = 0.107 m/s + Maximum Instantaneous TKE = 1.765 (m/s)^2 + Maximum Instantaneous CTKE = 0.971 (m/s)^2 + + +Grid Point Variance Summary: + + Y-coord -79.05 -74.40 -69.75 -65.10 -60.45 -55.80 -51.15 -46.50 -41.85 -37.20 -32.55 -27.90 -23.25 -18.60 -13.95 -9.30 -4.65 0.00 4.65 9.30 13.95 18.60 23.25 27.90 32.55 37.20 41.85 46.50 51.15 55.80 60.45 65.10 69.75 74.40 79.05 + + Height Standard deviation at grid points for the u component: + 168.40 0.512 0.504 0.500 0.531 0.480 0.476 0.465 0.461 0.479 0.468 0.449 0.478 0.496 0.504 0.490 0.538 0.516 0.531 0.544 0.527 0.480 0.474 0.521 0.554 0.539 0.555 0.525 0.544 0.524 0.546 0.569 0.574 0.565 0.510 0.487 + 163.75 0.562 0.509 0.528 0.534 0.489 0.461 0.457 0.466 0.467 0.526 0.522 0.504 0.519 0.531 0.523 0.508 0.540 0.551 0.557 0.538 0.504 0.513 0.520 0.543 0.530 0.556 0.573 0.548 0.519 0.553 0.542 0.535 0.550 0.539 0.520 + 159.10 0.568 0.534 0.569 0.566 0.475 0.453 0.483 0.454 0.475 0.509 0.508 0.505 0.520 0.523 0.531 0.535 0.566 0.537 0.551 0.518 0.547 0.514 0.512 0.537 0.534 0.537 0.533 0.556 0.562 0.545 0.543 0.546 0.569 0.516 0.539 + 154.45 0.540 0.533 0.553 0.556 0.458 0.428 0.433 0.474 0.449 0.506 0.520 0.456 0.450 0.489 0.484 0.520 0.521 0.533 0.542 0.551 0.524 0.526 0.528 0.536 0.553 0.524 0.506 0.496 0.509 0.555 0.540 0.567 0.559 0.496 0.496 + 149.80 0.536 0.512 0.569 0.526 0.499 0.448 0.419 0.499 0.494 0.500 0.478 0.495 0.434 0.474 0.481 0.517 0.504 0.475 0.507 0.533 0.501 0.512 0.515 0.517 0.512 0.531 0.481 0.475 0.502 0.494 0.522 0.549 0.568 0.564 0.505 + 145.15 0.517 0.552 0.573 0.533 0.474 0.449 0.435 0.491 0.493 0.465 0.456 0.454 0.469 0.470 0.497 0.513 0.521 0.518 0.475 0.513 0.493 0.475 0.489 0.556 0.521 0.481 0.463 0.440 0.490 0.463 0.462 0.489 0.521 0.540 0.524 + 140.50 0.548 0.512 0.553 0.536 0.468 0.469 0.488 0.500 0.495 0.493 0.489 0.473 0.500 0.510 0.506 0.506 0.525 0.510 0.508 0.495 0.525 0.516 0.524 0.509 0.474 0.459 0.459 0.453 0.469 0.480 0.476 0.484 0.460 0.505 0.534 + 135.85 0.547 0.552 0.541 0.556 0.497 0.501 0.482 0.484 0.538 0.563 0.514 0.486 0.492 0.505 0.492 0.474 0.509 0.507 0.556 0.540 0.549 0.556 0.558 0.482 0.462 0.477 0.472 0.459 0.399 0.426 0.481 0.446 0.455 0.471 0.538 + 131.20 0.521 0.524 0.514 0.527 0.507 0.522 0.522 0.539 0.528 0.541 0.536 0.478 0.477 0.480 0.466 0.483 0.510 0.543 0.536 0.512 0.536 0.572 0.561 0.535 0.479 0.467 0.454 0.438 0.418 0.414 0.455 0.447 0.457 0.488 0.517 + 126.55 0.516 0.507 0.539 0.549 0.528 0.503 0.542 0.560 0.560 0.539 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0.275 0.277 0.281 0.289 0.289 + 131.20 0.278 0.271 0.264 0.265 0.264 0.274 0.277 0.285 0.300 0.286 0.276 0.292 0.283 0.299 0.294 0.298 0.295 0.299 0.302 0.291 0.291 0.303 0.300 0.298 0.288 0.284 0.292 0.293 0.290 0.298 0.296 0.277 0.277 0.283 0.290 + 126.55 0.276 0.274 0.261 0.259 0.260 0.276 0.294 0.289 0.293 0.281 0.284 0.288 0.289 0.293 0.286 0.290 0.285 0.295 0.288 0.289 0.295 0.301 0.304 0.308 0.304 0.293 0.292 0.286 0.290 0.297 0.297 0.287 0.275 0.284 0.278 + 121.90 0.268 0.255 0.258 0.253 0.253 0.260 0.274 0.288 0.276 0.281 0.291 0.289 0.295 0.301 0.283 0.285 0.298 0.295 0.290 0.287 0.298 0.299 0.294 0.282 0.282 0.277 0.275 0.291 0.292 0.292 0.291 0.297 0.275 0.277 0.283 + 117.25 0.276 0.277 0.266 0.269 0.263 0.254 0.264 0.255 0.271 0.274 0.277 0.270 0.294 0.297 0.315 0.299 0.293 0.299 0.292 0.292 0.305 0.303 0.283 0.282 0.290 0.285 0.277 0.283 0.295 0.296 0.289 0.308 0.300 0.274 0.267 + 112.60 0.282 0.272 0.268 0.268 0.254 0.249 0.266 0.285 0.268 0.280 0.278 0.287 0.287 0.304 0.314 0.294 0.297 0.304 0.289 0.299 0.293 0.289 0.272 0.288 0.294 0.275 0.286 0.283 0.281 0.281 0.286 0.293 0.297 0.294 0.266 + 107.95 0.280 0.276 0.275 0.262 0.268 0.269 0.269 0.270 0.285 0.284 0.284 0.289 0.305 0.298 0.305 0.306 0.297 0.281 0.278 0.294 0.282 0.285 0.269 0.287 0.296 0.282 0.285 0.270 0.269 0.278 0.289 0.297 0.299 0.293 0.275 + 103.30 0.273 0.268 0.273 0.266 0.274 0.263 0.271 0.274 0.275 0.278 0.289 0.290 0.293 0.299 0.298 0.286 0.286 0.283 0.285 0.280 0.289 0.274 0.269 0.292 0.300 0.292 0.267 0.279 0.274 0.273 0.283 0.298 0.296 0.290 0.272 + 98.65 0.277 0.280 0.266 0.262 0.272 0.274 0.272 0.283 0.290 0.303 0.283 0.292 0.279 0.290 0.296 0.297 0.283 0.278 0.284 0.278 0.279 0.273 0.282 0.303 0.302 0.300 0.288 0.280 0.276 0.277 0.294 0.285 0.291 0.291 0.271 + 94.00 0.274 0.268 0.272 0.257 0.272 0.269 0.273 0.272 0.286 0.292 0.278 0.289 0.278 0.285 0.292 0.293 0.289 0.287 0.291 0.280 0.281 0.274 0.276 0.298 0.302 0.301 0.291 0.275 0.274 0.279 0.290 0.290 0.279 0.285 0.280 + 89.35 0.273 0.277 0.287 0.275 0.258 0.263 0.267 0.269 0.272 0.283 0.270 0.281 0.284 0.282 0.280 0.300 0.298 0.299 0.286 0.284 0.286 0.285 0.280 0.304 0.306 0.304 0.295 0.279 0.280 0.281 0.285 0.279 0.286 0.292 0.287 + 84.70 0.281 0.286 0.279 0.274 0.270 0.269 0.281 0.270 0.275 0.276 0.273 0.286 0.291 0.294 0.294 0.284 0.289 0.296 0.290 0.281 0.287 0.289 0.285 0.289 0.305 0.297 0.294 0.286 0.278 0.288 0.289 0.292 0.283 0.276 0.280 + 80.05 0.285 0.272 0.279 0.279 0.273 0.275 0.287 0.270 0.265 0.273 0.291 0.275 0.276 0.282 0.288 0.289 0.290 0.281 0.284 0.284 0.288 0.303 0.298 0.295 0.291 0.286 0.290 0.291 0.289 0.282 0.276 0.296 0.295 0.280 0.271 + 75.40 0.278 0.286 0.283 0.281 0.274 0.269 0.265 0.273 0.266 0.275 0.278 0.283 0.299 0.292 0.282 0.277 0.283 0.293 0.286 0.302 0.291 0.288 0.305 0.297 0.281 0.295 0.281 0.290 0.278 0.281 0.279 0.284 0.295 0.283 0.284 + 70.75 0.281 0.293 0.286 0.281 0.277 0.265 0.264 0.272 0.270 0.291 0.289 0.304 0.305 0.289 0.295 0.295 0.293 0.290 0.306 0.292 0.296 0.311 0.307 0.294 0.294 0.292 0.288 0.282 0.284 0.282 0.279 0.286 0.285 0.291 0.293 + 66.10 0.290 0.289 0.290 0.285 0.278 0.279 0.266 0.273 0.272 0.295 0.300 0.305 0.298 0.295 0.295 0.306 0.296 0.308 0.307 0.291 0.290 0.294 0.295 0.285 0.285 0.292 0.274 0.282 0.269 0.274 0.275 0.288 0.283 0.285 0.285 + 61.45 0.279 0.279 0.281 0.286 0.276 0.279 0.279 0.278 0.281 0.297 0.289 0.283 0.285 0.297 0.300 0.310 0.306 0.307 0.300 0.288 0.272 0.278 0.301 0.304 0.289 0.275 0.282 0.282 0.281 0.276 0.279 0.292 0.292 0.301 0.311 + 56.80 0.276 0.288 0.282 0.278 0.275 0.292 0.282 0.280 0.282 0.300 0.279 0.277 0.280 0.304 0.295 0.295 0.289 0.309 0.313 0.300 0.292 0.292 0.292 0.291 0.283 0.291 0.292 0.283 0.279 0.277 0.283 0.285 0.286 0.293 0.297 + 52.15 0.276 0.286 0.295 0.272 0.273 0.276 0.282 0.289 0.286 0.298 0.286 0.269 0.279 0.286 0.294 0.295 0.290 0.286 0.298 0.289 0.283 0.302 0.300 0.310 0.296 0.291 0.281 0.272 0.275 0.273 0.283 0.280 0.282 0.296 0.304 + 47.50 0.281 0.289 0.285 0.279 0.280 0.280 0.273 0.277 0.283 0.296 0.289 0.285 0.266 0.277 0.288 0.286 0.292 0.291 0.283 0.282 0.280 0.282 0.290 0.298 0.309 0.293 0.276 0.262 0.262 0.270 0.276 0.282 0.290 0.294 0.289 + 42.85 0.273 0.284 0.286 0.281 0.284 0.272 0.269 0.277 0.281 0.289 0.296 0.286 0.284 0.271 0.278 0.280 0.291 0.274 0.276 0.273 0.268 0.267 0.284 0.300 0.311 0.315 0.285 0.267 0.279 0.269 0.276 0.287 0.284 0.281 0.270 + 38.20 0.281 0.293 0.298 0.281 0.295 0.278 0.273 0.277 0.283 0.288 0.281 0.284 0.295 0.285 0.281 0.287 0.286 0.280 0.266 0.256 0.263 0.266 0.268 0.274 0.296 0.286 0.274 0.272 0.277 0.257 0.272 0.284 0.279 0.281 0.272 + 33.55 0.272 0.279 0.294 0.307 0.304 0.300 0.287 0.293 0.274 0.274 0.266 0.281 0.288 0.275 0.281 0.285 0.279 0.270 0.275 0.270 0.268 0.257 0.258 0.262 0.271 0.282 0.280 0.269 0.273 0.280 0.278 0.285 0.287 0.276 0.267 + 28.90 0.275 0.277 0.290 0.301 0.314 0.306 0.301 0.290 0.267 0.274 0.274 0.285 0.276 0.276 0.276 0.277 0.285 0.280 0.277 0.266 0.270 0.263 0.267 0.271 0.267 0.289 0.292 0.293 0.272 0.273 0.268 0.278 0.284 0.279 0.276 + 24.25 0.291 0.293 0.284 0.306 0.308 0.301 0.300 0.294 0.266 0.278 0.288 0.278 0.273 0.273 0.265 0.271 0.280 0.279 0.274 0.278 0.284 0.273 0.265 0.276 0.286 0.309 0.296 0.302 0.298 0.279 0.287 0.281 0.274 0.279 0.269 + 19.60 0.298 0.291 0.284 0.288 0.303 0.306 0.288 0.289 0.284 0.276 0.269 0.277 0.274 0.267 0.272 0.281 0.283 0.282 0.301 0.295 0.297 0.273 0.279 0.281 0.299 0.295 0.319 0.321 0.304 0.298 0.297 0.287 0.284 0.280 0.287 + 14.95 0.293 0.291 0.296 0.298 0.297 0.308 0.295 0.286 0.288 0.293 0.269 0.270 0.272 0.266 0.266 0.276 0.288 0.276 0.287 0.289 0.283 0.269 0.284 0.279 0.292 0.291 0.310 0.315 0.304 0.301 0.290 0.287 0.271 0.271 0.287 + 10.30 0.299 0.300 0.299 0.294 0.293 0.299 0.302 0.294 0.271 0.280 0.272 0.265 0.275 0.276 0.269 0.270 0.276 0.298 0.297 0.300 0.290 0.289 0.283 0.273 0.298 0.287 0.297 0.301 0.284 0.298 0.284 0.288 0.280 0.271 0.278 + 5.65 0.288 0.294 0.288 0.295 0.302 0.304 0.299 0.284 0.280 0.285 0.277 0.261 0.266 0.276 0.276 0.266 0.271 0.286 0.297 0.294 0.282 0.272 0.280 0.266 0.291 0.293 0.298 0.297 0.298 0.290 0.291 0.299 0.283 0.282 0.275 + 1.00 0.283 0.291 0.287 0.284 0.285 0.290 0.281 0.279 0.281 0.285 0.281 0.272 0.266 0.267 0.279 0.270 0.277 0.281 0.288 0.303 0.282 0.271 0.270 0.280 0.283 0.287 0.292 0.291 0.291 0.290 0.295 0.295 0.273 0.278 0.271 + + Mean standard deviation across all grid points: + u component: 0.507 m/s + v component: 0.473 m/s + w component: 0.283 m/s + + +U-component (X) statistics from the interpolated hub point: + + Mean = 8.0000 m/s + TI = 6.5657 % + + +Processing complete. 4107.5 CPU seconds used. diff --git a/examples/FAST.Farm_interface/inputs/FFFiles/TurbSim/HighT2.bts b/examples/FAST.Farm_interface/inputs/FFFiles/TurbSim/HighT2.bts new file mode 100644 index 00000000..801a4eca Binary files /dev/null and b/examples/FAST.Farm_interface/inputs/FFFiles/TurbSim/HighT2.bts differ diff --git a/examples/FAST.Farm_interface/inputs/FFFiles/TurbSim/HighT2.inp b/examples/FAST.Farm_interface/inputs/FFFiles/TurbSim/HighT2.inp new file mode 100644 index 00000000..24e9147c --- /dev/null +++ b/examples/FAST.Farm_interface/inputs/FFFiles/TurbSim/HighT2.inp @@ -0,0 +1,74 @@ +--------TurbSim v2.00.* Input File------------------------ +for Certification - Test #1 (Kaimal Spectrum, formatted FF files). +---------Runtime Options----------------------------------- +False Echo - Echo input data to .ech (flag) +-281629 RandSeed1 - First random seed (-2147483648 to 2147483647) +RanLux RandSeed2 - Second random seed (-2147483648 to 2147483647) for intrinsic pRNG, or an alternative pRNG: "RanLux" or "RNSNLW" +False WrBHHTP - Output hub-height turbulence parameters in binary form? (Generates RootName.bin) +False WrFHHTP - Output hub-height turbulence parameters in formatted form? (Generates RootName.dat) +False WrADHH - Output hub-height time-series data in AeroDyn form? (Generates RootName.hh) +True WrADFF - Output full-field time-series data in TurbSim/AeroDyn form? (Generates RootName.bts) +False WrBLFF - Output full-field time-series data in BLADED/AeroDyn form? (Generates RootName.wnd) +False WrADTWR - Output tower time-series data? (Generates RootName.twr) +False WrFMTFF - Output full-field time-series data in formatted (readable) form? (Generates RootName.u, RootName.v, RootName.w) +False WrACT - Output coherent turbulence time steps in AeroDyn form? (Generates RootName.cts) +True Clockwise - Clockwise rotation looking downwind? (used only for full-field binary files - not necessary for AeroDyn) +0 ScaleIEC - Scale IEC turbulence models to exact target standard deviation? [0=no additional scaling; 1=use hub scale uniformly; 2=use individual scales] + +--------Turbine/Model Specifications----------------------- +37 NumGrid_Z - Vertical grid-point matrix dimension +35 NumGrid_Y - Horizontal grid-point matrix dimension +0.25 TimeStep - Time step [seconds] +600.0 AnalysisTime - Length of analysis time series [seconds] (program will add time if necessary: AnalysisTime = MAX(AnalysisTime, UsableTime+GridWidth/MeanHHWS) ) +"ALL" UsableTime - Usable length of output time series [seconds] (program will add GridWidth/MeanHHWS seconds unless UsableTime is "ALL") +89.35 HubHt - Hub height [m] (should be > 0.5*GridHeight) +167.4 GridHeight - Grid height [m] +158.1 GridWidth - Grid width [m] (should be >= 2*(RotorRadius+ShaftLength)) +0 VFlowAng - Vertical mean flow (uptilt) angle [degrees] +0 HFlowAng - Horizontal mean flow (skew) angle [degrees] + +--------Meteorological Boundary Conditions------------------- +"TIMESR" TurbModel - Turbulence model ("IECKAI","IECVKM","GP_LLJ","NWTCUP","SMOOTH","WF_UPW","WF_07D","WF_14D","TIDAL","API","USRINP","TIMESR", or "NONE") +"USRTimeSeries_T2.txt" UserFile - Name of the file that contains inputs for user-defined spectra or time series inputs (used only for "IECKAI" and "TIMESR" models) +1 IECstandard - Number of IEC 61400-x standard (x=1,2, or 3 with optional 61400-1 edition number (i.e. "1-Ed2") ) +"8.000 " IECturbc - IEC turbulence characteristic ("A", "B", "C" or the turbulence intensity in percent) ("KHTEST" option with NWTCUP model, not used for other models) +"NTM" IEC_WindType - IEC turbulence type ("NTM"=normal, "xETM"=extreme turbulence, "xEWM1"=extreme 1-year wind, "xEWM50"=extreme 50-year wind, where x=wind turbine class 1, 2, or 3) +"default" ETMc - IEC Extreme Turbulence Model "c" parameter [m/s] +"PL" WindProfileType - Velocity profile type ("LOG";"PL"=power law;"JET";"H2L"=Log law for TIDAL model;"API";"PL";"TS";"IEC"=PL on rotor disk, LOG elsewhere; or "default") +"unused" ProfileFile - Name of the file that contains input profiles for WindProfileType="USR" and/or TurbModel="USRVKM" [-] +90 RefHt - Height of the reference velocity (URef) [m] +8.0 URef - Mean (total) velocity at the reference height [m/s] (or "default" for JET velocity profile) [must be 1-hr mean for API model; otherwise is the mean over AnalysisTime seconds] +350 ZJetMax - Jet height [m] (used only for JET velocity profile, valid 70-490 m) +0.0 PLExp - Power law exponent [-] (or "default") +"default" Z0 - Surface roughness length [m] (or "default") + +--------Non-IEC Meteorological Boundary Conditions------------ +"default" Latitude - Site latitude [degrees] (or "default") +0.05 RICH_NO - Gradient Richardson number [-] +"default" UStar - Friction or shear velocity [m/s] (or "default") +"default" ZI - Mixing layer depth [m] (or "default") +"default" PC_UW - Hub mean u'w' Reynolds stress [m^2/s^2] (or "default" or "none") +"default" PC_UV - Hub mean u'v' Reynolds stress [m^2/s^2] (or "default" or "none") +"default" PC_VW - Hub mean v'w' Reynolds stress [m^2/s^2] (or "default" or "none") + +--------Spatial Coherence Parameters---------------------------- +"IEC" SCMod1 - u-component coherence model ("GENERAL","IEC","API","NONE", or "default") +"IEC" SCMod2 - v-component coherence model ("GENERAL","IEC","NONE", or "default") +"IEC" SCMod3 - w-component coherence model ("GENERAL","IEC","NONE", or "default") +"12 0.00035273" InCDec1 - u-component coherence parameters for general or IEC models [-, m^-1] (e.g. "10.0 0.3e-3" in quotes) (or "default") +"12 0.00035273" InCDec2 - v-component coherence parameters for general or IEC models [-, m^-1] (e.g. "10.0 0.3e-3" in quotes) (or "default") +"12 0.00035273" InCDec3 - w-component coherence parameters for general or IEC models [-, m^-1] (e.g. "10.0 0.3e-3" in quotes) (or "default") +"0.0" CohExp - Coherence exponent for general model [-] (or "default") + +--------Coherent Turbulence Scaling Parameters------------------- +".\EventData" CTEventPath - Name of the path where event data files are located +"random" CTEventFile - Type of event files ("LES", "DNS", or "RANDOM") +True Randomize - Randomize the disturbance scale and locations? (true/false) +1 DistScl - Disturbance scale [-] (ratio of event dataset height to rotor disk). (Ignored when Randomize = true.) +0.5 CTLy - Fractional location of tower centerline from right [-] (looking downwind) to left side of the dataset. (Ignored when Randomize = true.) +0.5 CTLz - Fractional location of hub height from the bottom of the dataset. [-] (Ignored when Randomize = true.) +30 CTStartTime - Minimum start time for coherent structures in RootName.cts [seconds] + +==================================================== +! NOTE: Do not add or remove any lines in this file! +==================================================== \ No newline at end of file diff --git a/examples/FAST.Farm_interface/inputs/FFFiles/TurbSim/HighT2.sum b/examples/FAST.Farm_interface/inputs/FFFiles/TurbSim/HighT2.sum new file mode 100644 index 00000000..f19d6e35 --- /dev/null +++ b/examples/FAST.Farm_interface/inputs/FFFiles/TurbSim/HighT2.sum @@ -0,0 +1,331 @@ + +This summary file was generated by TurbSim (from OpenFAST-v3.5.3) on 20-Jun-2024 at 17:22:54. + + +Runtime Options: + + -281629 Random seed #1 + RANLUX Type of random number generator + F Output binary HH turbulence parameters? + F Output formatted turbulence parameters? + F Output AeroDyn HH files? + T Output AeroDyn FF files? + F Output BLADED FF files? + F Output tower data? + F Output HAWC FF files? + F Output formatted FF files? + T Output coherent turbulence time step file? + 0 - NONE IEC turbulence models scaled to exact specified standard deviation + + +Turbine/Model Specifications: + + 37 Vertical grid-point matrix dimension + 35 Horizontal grid-point matrix dimension + 0.250 Time step [seconds] + 600.000 Analysis time [seconds] + 600.000 Usable output time [seconds] + 89.350 Hub height [m] + 167.400 Grid height [m] + 158.100 Grid width [m] + 0.000 Vertical flow angle [degrees] + 0.000 Horizontal flow angle [degrees] + + +Meteorological Boundary Conditions: + + TIMESR User-input time series spectral model + N/A IEC standard + N/A IEC turbulence characteristic + N/A IEC turbulence type + N/A IEC Extreme Turbulence Model (ETM) "c" parameter [m/s] + PL Wind profile type + 90.000 Reference height [m] + 8.000 Reference wind speed [m/s] + N/A Jet height [m] + 0.000 Power law exponent + 0.030 Surface roughness length [m] + + +Non-IEC Meteorological Boundary Conditions: + + 45.000 Site latitude [degrees] + 0.050 Gradient Richardson number + 0.384 Friction or shear velocity [m/s] + N/A Mixing layer depth [m] + N/A Mean hub u'w' Reynolds stress + N/A Mean hub u'v' Reynolds stress + N/A Mean hub v'w' Reynolds stress + + +Spatial Coherence Models: + + IEC u-component coherence model + IEC v-component coherence model + IEC w-component coherence model +( 12.000, 0.353E-03) u-component coherence parameters +( 12.000, 0.353E-03) v-component coherence parameters +( 12.000, 0.353E-03) w-component coherence parameters + N/A Coherence exponent + + +Coherent Turbulence Scaling Parameters: + +.\EventData + Name of the path containing the coherent turbulence data files + dns Type of coherent turbulence data files + 1.000 Disturbance scale (ratio of wave height to rotor diameter) + 0.500 Fractional location of tower centerline from right + 0.500 Fractional location of hub height from the bottom of the dataset + 30.000 Minimum start time for coherent structures [seconds] + + +Profiles from User-Defined Time-Series Input: + + Height Wind Speed Horizontal Angle Vertical Angle + (m) (m/s) (deg) (deg) + ------ ---------- ---------------- -------------- + 94.00 8.00 0.00 0.00 + + +You have requested that the following file(s) be generated: + + ../FFSim/Cond00_v08.0_PL0.0_TI8/Case0_wdirp00/Seed_0/TurbSim/HighT2.bts (AeroDyn/TurbSim full-field wind file) + + +Turbulence Simulation Scaling Parameter Summary: + + Turbulence model used = User-input time series + Gradient Richardson number = 0.050 + Monin-Obukhov (M-O) z/L parameter = 0.067 + Monin-Obukhov (M-O) length scale = 1340.250 m + Mean wind speed at hub height = 8.000 m/s + + Wind profile type = Power law + Power law exponent = 0.000 + Mean shear across rotor disk = 0.000 (m/s)/m + Assumed rotor diameter = 158.100 m + Surface roughness length = 0.030 m + + Nyquist frequency of turbulent wind field = 2.000 Hz + + Number of time steps in the FFT = 2400 + Number of time steps output = 2400 + Number of points simulated = 1295 + + +Mean Flow Angles: + + Vertical = 0.0 degrees + Horizontal = 0.0 degrees + +Mean Wind Speed Profile: + + Height Wind Speed Horizontal Angle Vertical Angle U-comp (X) V-comp (Y) W-comp (Z) + (m) (m/s) (degrees) (degrees) (m/s) (m/s) (m/s) + ------ ---------- ---------------- -------------- ---------- ---------- ---------- + 168.4 8.00 0.00 0.00 8.00 0.00 0.00 + 163.7 8.00 0.00 0.00 8.00 0.00 0.00 + 159.1 8.00 0.00 0.00 8.00 0.00 0.00 + 154.4 8.00 0.00 0.00 8.00 0.00 0.00 + 149.8 8.00 0.00 0.00 8.00 0.00 0.00 + 145.1 8.00 0.00 0.00 8.00 0.00 0.00 + 140.5 8.00 0.00 0.00 8.00 0.00 0.00 + 135.8 8.00 0.00 0.00 8.00 0.00 0.00 + 131.2 8.00 0.00 0.00 8.00 0.00 0.00 + 126.5 8.00 0.00 0.00 8.00 0.00 0.00 + 121.9 8.00 0.00 0.00 8.00 0.00 0.00 + 117.2 8.00 0.00 0.00 8.00 0.00 0.00 + 112.6 8.00 0.00 0.00 8.00 0.00 0.00 + 107.9 8.00 0.00 0.00 8.00 0.00 0.00 + 103.3 8.00 0.00 0.00 8.00 0.00 0.00 + 98.6 8.00 0.00 0.00 8.00 0.00 0.00 + 94.0 8.00 0.00 0.00 8.00 0.00 0.00 + 89.3 8.00 0.00 0.00 8.00 0.00 0.00 + 84.7 8.00 0.00 0.00 8.00 0.00 0.00 + 80.0 8.00 0.00 0.00 8.00 0.00 0.00 + 75.4 8.00 0.00 0.00 8.00 0.00 0.00 + 70.7 8.00 0.00 0.00 8.00 0.00 0.00 + 66.1 8.00 0.00 0.00 8.00 0.00 0.00 + 61.4 8.00 0.00 0.00 8.00 0.00 0.00 + 56.8 8.00 0.00 0.00 8.00 0.00 0.00 + 52.1 8.00 0.00 0.00 8.00 0.00 0.00 + 47.5 8.00 0.00 0.00 8.00 0.00 0.00 + 42.8 8.00 0.00 0.00 8.00 0.00 0.00 + 38.2 8.00 0.00 0.00 8.00 0.00 0.00 + 33.5 8.00 0.00 0.00 8.00 0.00 0.00 + 28.9 8.00 0.00 0.00 8.00 0.00 0.00 + 24.2 8.00 0.00 0.00 8.00 0.00 0.00 + 19.6 8.00 0.00 0.00 8.00 0.00 0.00 + 14.9 8.00 0.00 0.00 8.00 0.00 0.00 + 10.3 8.00 0.00 0.00 8.00 0.00 0.00 + 5.6 8.00 0.00 0.00 8.00 0.00 0.00 + 1.0 8.00 0.00 0.00 8.00 0.00 0.00 + + +Harvested Random Seeds after Generation of the Random Numbers: + + 43317750 K 1 + 0 K 2 + + +Hub-Height Simulated Turbulence Statistical Summary: + + Type of Wind Min (m/s) Mean (m/s) Max (m/s) Sigma (m/s) TI (%) + ---------------- --------- ---------- --------- ----------- ------ + Longitudinal (u) 6.52 8.00 9.42 0.552 6.896 + Lateral (v) -1.72 -0.00 1.21 0.508 6.355 + Vertical (w) -0.88 0.00 0.98 0.289 3.615 + U component 6.52 8.00 9.42 0.552 6.896 + V component -1.72 -0.00 1.21 0.508 6.355 + W component -0.88 0.00 0.98 0.289 3.615 + Horizontal (U&V) 6.53 8.02 9.47 0.552 6.882 + Total 6.54 8.02 9.47 0.550 6.862 + + Min Reynolds Mean Reynolds Max Reynolds Correlation + Product Stress (m/s)^2 Stress (m/s)^2 Stress (m/s)^2 Coefficient + ---------------- -------------- -------------- -------------- ----------- + u'w' -0.759 0.007 0.910 0.041 + u'v' -1.491 -0.040 1.035 -0.143 + v'w' -0.724 -0.007 0.702 -0.046 + + + Friction Velocity (Ustar) = 0.081 m/s + Maximum Instantaneous TKE = 1.679 (m/s)^2 + Maximum Instantaneous CTKE = 0.748 (m/s)^2 + + +Grid Point Variance Summary: + + Y-coord -79.05 -74.40 -69.75 -65.10 -60.45 -55.80 -51.15 -46.50 -41.85 -37.20 -32.55 -27.90 -23.25 -18.60 -13.95 -9.30 -4.65 0.00 4.65 9.30 13.95 18.60 23.25 27.90 32.55 37.20 41.85 46.50 51.15 55.80 60.45 65.10 69.75 74.40 79.05 + + Height Standard deviation at grid points for the u component: + 168.40 0.564 0.566 0.550 0.604 0.536 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0.281 0.269 0.276 0.291 0.287 0.278 0.279 0.294 0.299 0.302 0.293 0.283 0.289 0.275 0.299 0.294 0.299 0.295 0.295 0.290 0.289 0.296 0.282 0.282 0.278 + 1.00 0.286 0.289 0.289 0.287 0.286 0.291 0.280 0.281 0.282 0.287 0.287 0.279 0.273 0.275 0.291 0.283 0.287 0.290 0.290 0.307 0.290 0.282 0.279 0.291 0.291 0.290 0.291 0.290 0.288 0.290 0.291 0.292 0.276 0.281 0.276 + + Mean standard deviation across all grid points: + u component: 0.545 m/s + v component: 0.476 m/s + w component: 0.286 m/s + + +U-component (X) statistics from the interpolated hub point: + + Mean = 8.0000 m/s + TI = 6.8961 % + + +Processing complete. 4023.6 CPU seconds used. diff --git a/examples/FAST.Farm_interface/inputs/FFFiles/TurbSim/HighT3.bts b/examples/FAST.Farm_interface/inputs/FFFiles/TurbSim/HighT3.bts new file mode 100644 index 00000000..ea359b3d Binary files /dev/null and b/examples/FAST.Farm_interface/inputs/FFFiles/TurbSim/HighT3.bts differ diff --git a/examples/FAST.Farm_interface/inputs/FFFiles/TurbSim/HighT3.inp b/examples/FAST.Farm_interface/inputs/FFFiles/TurbSim/HighT3.inp new file mode 100644 index 00000000..b6166971 --- /dev/null +++ b/examples/FAST.Farm_interface/inputs/FFFiles/TurbSim/HighT3.inp @@ -0,0 +1,74 @@ +--------TurbSim v2.00.* Input File------------------------ +for Certification - Test #1 (Kaimal Spectrum, formatted FF files). +---------Runtime Options----------------------------------- +False Echo - Echo input data to .ech (flag) +-281629 RandSeed1 - First random seed (-2147483648 to 2147483647) +RanLux RandSeed2 - Second random seed (-2147483648 to 2147483647) for intrinsic pRNG, or an alternative pRNG: "RanLux" or "RNSNLW" +False WrBHHTP - Output hub-height turbulence parameters in binary form? (Generates RootName.bin) +False WrFHHTP - Output hub-height turbulence parameters in formatted form? (Generates RootName.dat) +False WrADHH - Output hub-height time-series data in AeroDyn form? (Generates RootName.hh) +True WrADFF - Output full-field time-series data in TurbSim/AeroDyn form? (Generates RootName.bts) +False WrBLFF - Output full-field time-series data in BLADED/AeroDyn form? (Generates RootName.wnd) +False WrADTWR - Output tower time-series data? (Generates RootName.twr) +False WrFMTFF - Output full-field time-series data in formatted (readable) form? (Generates RootName.u, RootName.v, RootName.w) +False WrACT - Output coherent turbulence time steps in AeroDyn form? (Generates RootName.cts) +True Clockwise - Clockwise rotation looking downwind? (used only for full-field binary files - not necessary for AeroDyn) +0 ScaleIEC - Scale IEC turbulence models to exact target standard deviation? [0=no additional scaling; 1=use hub scale uniformly; 2=use individual scales] + +--------Turbine/Model Specifications----------------------- +37 NumGrid_Z - Vertical grid-point matrix dimension +35 NumGrid_Y - Horizontal grid-point matrix dimension +0.25 TimeStep - Time step [seconds] +600.0 AnalysisTime - Length of analysis time series [seconds] (program will add time if necessary: AnalysisTime = MAX(AnalysisTime, UsableTime+GridWidth/MeanHHWS) ) +"ALL" UsableTime - Usable length of output time series [seconds] (program will add GridWidth/MeanHHWS seconds unless UsableTime is "ALL") +89.35 HubHt - Hub height [m] (should be > 0.5*GridHeight) +167.4 GridHeight - Grid height [m] +158.1 GridWidth - Grid width [m] (should be >= 2*(RotorRadius+ShaftLength)) +0 VFlowAng - Vertical mean flow (uptilt) angle [degrees] +0 HFlowAng - Horizontal mean flow (skew) angle [degrees] + +--------Meteorological Boundary Conditions------------------- +"TIMESR" TurbModel - Turbulence model ("IECKAI","IECVKM","GP_LLJ","NWTCUP","SMOOTH","WF_UPW","WF_07D","WF_14D","TIDAL","API","USRINP","TIMESR", or "NONE") +"USRTimeSeries_T3.txt" UserFile - Name of the file that contains inputs for user-defined spectra or time series inputs (used only for "IECKAI" and "TIMESR" models) +1 IECstandard - Number of IEC 61400-x standard (x=1,2, or 3 with optional 61400-1 edition number (i.e. "1-Ed2") ) +"8.000 " IECturbc - IEC turbulence characteristic ("A", "B", "C" or the turbulence intensity in percent) ("KHTEST" option with NWTCUP model, not used for other models) +"NTM" IEC_WindType - IEC turbulence type ("NTM"=normal, "xETM"=extreme turbulence, "xEWM1"=extreme 1-year wind, "xEWM50"=extreme 50-year wind, where x=wind turbine class 1, 2, or 3) +"default" ETMc - IEC Extreme Turbulence Model "c" parameter [m/s] +"PL" WindProfileType - Velocity profile type ("LOG";"PL"=power law;"JET";"H2L"=Log law for TIDAL model;"API";"PL";"TS";"IEC"=PL on rotor disk, LOG elsewhere; or "default") +"unused" ProfileFile - Name of the file that contains input profiles for WindProfileType="USR" and/or TurbModel="USRVKM" [-] +90 RefHt - Height of the reference velocity (URef) [m] +8.0 URef - Mean (total) velocity at the reference height [m/s] (or "default" for JET velocity profile) [must be 1-hr mean for API model; otherwise is the mean over AnalysisTime seconds] +350 ZJetMax - Jet height [m] (used only for JET velocity profile, valid 70-490 m) +0.0 PLExp - Power law exponent [-] (or "default") +"default" Z0 - Surface roughness length [m] (or "default") + +--------Non-IEC Meteorological Boundary Conditions------------ +"default" Latitude - Site latitude [degrees] (or "default") +0.05 RICH_NO - Gradient Richardson number [-] +"default" UStar - Friction or shear velocity [m/s] (or "default") +"default" ZI - Mixing layer depth [m] (or "default") +"default" PC_UW - Hub mean u'w' Reynolds stress [m^2/s^2] (or "default" or "none") +"default" PC_UV - Hub mean u'v' Reynolds stress [m^2/s^2] (or "default" or "none") +"default" PC_VW - Hub mean v'w' Reynolds stress [m^2/s^2] (or "default" or "none") + +--------Spatial Coherence Parameters---------------------------- +"IEC" SCMod1 - u-component coherence model ("GENERAL","IEC","API","NONE", or "default") +"IEC" SCMod2 - v-component coherence model ("GENERAL","IEC","NONE", or "default") +"IEC" SCMod3 - w-component coherence model ("GENERAL","IEC","NONE", or "default") +"12 0.00035273" InCDec1 - u-component coherence parameters for general or IEC models [-, m^-1] (e.g. "10.0 0.3e-3" in quotes) (or "default") +"12 0.00035273" InCDec2 - v-component coherence parameters for general or IEC models [-, m^-1] (e.g. "10.0 0.3e-3" in quotes) (or "default") +"12 0.00035273" InCDec3 - w-component coherence parameters for general or IEC models [-, m^-1] (e.g. "10.0 0.3e-3" in quotes) (or "default") +"0.0" CohExp - Coherence exponent for general model [-] (or "default") + +--------Coherent Turbulence Scaling Parameters------------------- +".\EventData" CTEventPath - Name of the path where event data files are located +"random" CTEventFile - Type of event files ("LES", "DNS", or "RANDOM") +True Randomize - Randomize the disturbance scale and locations? (true/false) +1 DistScl - Disturbance scale [-] (ratio of event dataset height to rotor disk). (Ignored when Randomize = true.) +0.5 CTLy - Fractional location of tower centerline from right [-] (looking downwind) to left side of the dataset. (Ignored when Randomize = true.) +0.5 CTLz - Fractional location of hub height from the bottom of the dataset. [-] (Ignored when Randomize = true.) +30 CTStartTime - Minimum start time for coherent structures in RootName.cts [seconds] + +==================================================== +! NOTE: Do not add or remove any lines in this file! +==================================================== \ No newline at end of file diff --git a/examples/FAST.Farm_interface/inputs/FFFiles/TurbSim/HighT3.sum b/examples/FAST.Farm_interface/inputs/FFFiles/TurbSim/HighT3.sum new file mode 100644 index 00000000..9a7e5d33 --- /dev/null +++ b/examples/FAST.Farm_interface/inputs/FFFiles/TurbSim/HighT3.sum @@ -0,0 +1,331 @@ + +This summary file was generated by TurbSim (from OpenFAST-v3.5.3) on 20-Jun-2024 at 17:23:35. + + +Runtime Options: + + -281629 Random seed #1 + RANLUX Type of random number generator + F Output binary HH turbulence parameters? + F Output formatted turbulence parameters? + F Output AeroDyn HH files? + T Output AeroDyn FF files? + F Output BLADED FF files? + F Output tower data? + F Output HAWC FF files? + F Output formatted FF files? + T Output coherent turbulence time step file? + 0 - NONE IEC turbulence models scaled to exact specified standard deviation + + +Turbine/Model Specifications: + + 37 Vertical grid-point matrix dimension + 35 Horizontal grid-point matrix dimension + 0.250 Time step [seconds] + 600.000 Analysis time [seconds] + 600.000 Usable output time [seconds] + 89.350 Hub height [m] + 167.400 Grid height [m] + 158.100 Grid width [m] + 0.000 Vertical flow angle [degrees] + 0.000 Horizontal flow angle [degrees] + + +Meteorological Boundary Conditions: + + TIMESR User-input time series spectral model + N/A IEC standard + N/A IEC turbulence characteristic + N/A IEC turbulence type + N/A IEC Extreme Turbulence Model (ETM) "c" parameter [m/s] + PL Wind profile type + 90.000 Reference height [m] + 8.000 Reference wind speed [m/s] + N/A Jet height [m] + 0.000 Power law exponent + 0.030 Surface roughness length [m] + + +Non-IEC Meteorological Boundary Conditions: + + 45.000 Site latitude [degrees] + 0.050 Gradient Richardson number + 0.384 Friction or shear velocity [m/s] + N/A Mixing layer depth [m] + N/A Mean hub u'w' Reynolds stress + N/A Mean hub u'v' Reynolds stress + N/A Mean hub v'w' Reynolds stress + + +Spatial Coherence Models: + + IEC u-component coherence model + IEC v-component coherence model + IEC w-component coherence model +( 12.000, 0.353E-03) u-component coherence parameters +( 12.000, 0.353E-03) v-component coherence parameters +( 12.000, 0.353E-03) w-component coherence parameters + N/A Coherence exponent + + +Coherent Turbulence Scaling Parameters: + +.\EventData + Name of the path containing the coherent turbulence data files + dns Type of coherent turbulence data files + 1.000 Disturbance scale (ratio of wave height to rotor diameter) + 0.500 Fractional location of tower centerline from right + 0.500 Fractional location of hub height from the bottom of the dataset + 30.000 Minimum start time for coherent structures [seconds] + + +Profiles from User-Defined Time-Series Input: + + Height Wind Speed Horizontal Angle Vertical Angle + (m) (m/s) (deg) (deg) + ------ ---------- ---------------- -------------- + 94.00 8.00 0.00 0.00 + + +You have requested that the following file(s) be generated: + + ../FFSim/Cond00_v08.0_PL0.0_TI8/Case0_wdirp00/Seed_0/TurbSim/HighT3.bts (AeroDyn/TurbSim full-field wind file) + + +Turbulence Simulation Scaling Parameter Summary: + + Turbulence model used = User-input time series + Gradient Richardson number = 0.050 + Monin-Obukhov (M-O) z/L parameter = 0.067 + Monin-Obukhov (M-O) length scale = 1340.250 m + Mean wind speed at hub height = 8.000 m/s + + Wind profile type = Power law + Power law exponent = 0.000 + Mean shear across rotor disk = 0.000 (m/s)/m + Assumed rotor diameter = 158.100 m + Surface roughness length = 0.030 m + + Nyquist frequency of turbulent wind field = 2.000 Hz + + Number of time steps in the FFT = 2400 + Number of time steps output = 2400 + Number of points simulated = 1295 + + +Mean Flow Angles: + + Vertical = 0.0 degrees + Horizontal = 0.0 degrees + +Mean Wind Speed Profile: + + Height Wind Speed Horizontal Angle Vertical Angle U-comp (X) V-comp (Y) W-comp (Z) + (m) (m/s) (degrees) (degrees) (m/s) (m/s) (m/s) + ------ ---------- ---------------- -------------- ---------- ---------- ---------- + 168.4 8.00 0.00 0.00 8.00 0.00 0.00 + 163.7 8.00 0.00 0.00 8.00 0.00 0.00 + 159.1 8.00 0.00 0.00 8.00 0.00 0.00 + 154.4 8.00 0.00 0.00 8.00 0.00 0.00 + 149.8 8.00 0.00 0.00 8.00 0.00 0.00 + 145.1 8.00 0.00 0.00 8.00 0.00 0.00 + 140.5 8.00 0.00 0.00 8.00 0.00 0.00 + 135.8 8.00 0.00 0.00 8.00 0.00 0.00 + 131.2 8.00 0.00 0.00 8.00 0.00 0.00 + 126.5 8.00 0.00 0.00 8.00 0.00 0.00 + 121.9 8.00 0.00 0.00 8.00 0.00 0.00 + 117.2 8.00 0.00 0.00 8.00 0.00 0.00 + 112.6 8.00 0.00 0.00 8.00 0.00 0.00 + 107.9 8.00 0.00 0.00 8.00 0.00 0.00 + 103.3 8.00 0.00 0.00 8.00 0.00 0.00 + 98.6 8.00 0.00 0.00 8.00 0.00 0.00 + 94.0 8.00 0.00 0.00 8.00 0.00 0.00 + 89.3 8.00 0.00 0.00 8.00 0.00 0.00 + 84.7 8.00 0.00 0.00 8.00 0.00 0.00 + 80.0 8.00 0.00 0.00 8.00 0.00 0.00 + 75.4 8.00 0.00 0.00 8.00 0.00 0.00 + 70.7 8.00 0.00 0.00 8.00 0.00 0.00 + 66.1 8.00 0.00 0.00 8.00 0.00 0.00 + 61.4 8.00 0.00 0.00 8.00 0.00 0.00 + 56.8 8.00 0.00 0.00 8.00 0.00 0.00 + 52.1 8.00 0.00 0.00 8.00 0.00 0.00 + 47.5 8.00 0.00 0.00 8.00 0.00 0.00 + 42.8 8.00 0.00 0.00 8.00 0.00 0.00 + 38.2 8.00 0.00 0.00 8.00 0.00 0.00 + 33.5 8.00 0.00 0.00 8.00 0.00 0.00 + 28.9 8.00 0.00 0.00 8.00 0.00 0.00 + 24.2 8.00 0.00 0.00 8.00 0.00 0.00 + 19.6 8.00 0.00 0.00 8.00 0.00 0.00 + 14.9 8.00 0.00 0.00 8.00 0.00 0.00 + 10.3 8.00 0.00 0.00 8.00 0.00 0.00 + 5.6 8.00 0.00 0.00 8.00 0.00 0.00 + 1.0 8.00 0.00 0.00 8.00 0.00 0.00 + + +Harvested Random Seeds after Generation of the Random Numbers: + + 43317750 K 1 + 0 K 2 + + +Hub-Height Simulated Turbulence Statistical Summary: + + Type of Wind Min (m/s) Mean (m/s) Max (m/s) Sigma (m/s) TI (%) + ---------------- --------- ---------- --------- ----------- ------ + Longitudinal (u) 6.42 8.00 9.32 0.504 6.295 + Lateral (v) -1.27 -0.00 1.48 0.493 6.162 + Vertical (w) -0.95 -0.00 1.19 0.290 3.622 + U component 6.42 8.00 9.32 0.504 6.295 + V component -1.27 -0.00 1.48 0.493 6.162 + W component -0.95 -0.00 1.19 0.290 3.622 + Horizontal (U&V) 6.42 8.02 9.35 0.503 6.279 + Total 6.43 8.02 9.35 0.502 6.261 + + Min Reynolds Mean Reynolds Max Reynolds Correlation + Product Stress (m/s)^2 Stress (m/s)^2 Stress (m/s)^2 Coefficient + ---------------- -------------- -------------- -------------- ----------- + u'w' -0.821 0.008 0.676 0.053 + u'v' -1.138 -0.022 1.066 -0.087 + v'w' -0.579 -0.004 1.034 -0.029 + + + Friction Velocity (Ustar) = 0.088 m/s + Maximum Instantaneous TKE = 1.326 (m/s)^2 + Maximum Instantaneous CTKE = 0.570 (m/s)^2 + + +Grid Point Variance Summary: + + Y-coord -79.05 -74.40 -69.75 -65.10 -60.45 -55.80 -51.15 -46.50 -41.85 -37.20 -32.55 -27.90 -23.25 -18.60 -13.95 -9.30 -4.65 0.00 4.65 9.30 13.95 18.60 23.25 27.90 32.55 37.20 41.85 46.50 51.15 55.80 60.45 65.10 69.75 74.40 79.05 + + Height Standard deviation at grid points for the u component: + 168.40 0.518 0.502 0.474 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0.281 0.286 0.282 0.271 0.277 0.285 0.281 0.274 0.273 0.284 0.291 0.293 0.285 0.276 0.284 0.275 0.297 0.296 0.302 0.300 0.299 0.297 0.300 0.306 0.290 0.289 0.278 + 1.00 0.285 0.289 0.290 0.290 0.287 0.297 0.283 0.284 0.286 0.292 0.288 0.281 0.276 0.271 0.282 0.275 0.280 0.283 0.283 0.302 0.282 0.276 0.276 0.287 0.290 0.290 0.295 0.291 0.290 0.294 0.298 0.299 0.284 0.287 0.278 + + Mean standard deviation across all grid points: + u component: 0.470 m/s + v component: 0.488 m/s + w component: 0.285 m/s + + +U-component (X) statistics from the interpolated hub point: + + Mean = 8.0000 m/s + TI = 6.2948 % + + +Processing complete. 3661.7 CPU seconds used. diff --git a/examples/FAST.Farm_interface/inputs/FFFiles/TurbSim/Low.bts b/examples/FAST.Farm_interface/inputs/FFFiles/TurbSim/Low.bts new file mode 100644 index 00000000..298b1233 Binary files /dev/null and b/examples/FAST.Farm_interface/inputs/FFFiles/TurbSim/Low.bts differ diff --git a/examples/FAST.Farm_interface/inputs/FFFiles/TurbSim/USRTimeSeries_T1.txt b/examples/FAST.Farm_interface/inputs/FFFiles/TurbSim/USRTimeSeries_T1.txt new file mode 100644 index 00000000..c788c579 --- /dev/null +++ b/examples/FAST.Farm_interface/inputs/FFFiles/TurbSim/USRTimeSeries_T1.txt @@ -0,0 +1,2412 @@ +--------------TurbSim v2.00.* User Time Series Input File----------------------- + Time series input from low-res turbsim run +-------------------------------------------------------------------------------- + 3 nComp - Number of velocity components in the file + 1 nPoints - Number of time series points contained in this file (-) + 1 RefPtID - Index of the reference point (1-nPoints) + Pointyi Pointzi ! nPoints listed in order of increasing height + (m) (m) + 0.00000 94.00000 +--------Time Series------------------------------------------------------------- +Elapsed Time Point01u Point01v Point01w + (s) (m/s) (m/s) (m/s) + 0.00 7.33551 -0.23094 -0.18196 + 0.25 7.25104 -0.26815 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593.75 7.49238 0.18483 -0.29336 + 594.00 7.30934 0.30613 -0.42095 + 594.25 7.29507 0.42928 -0.55800 + 594.50 7.11290 -0.07642 -0.31559 + 594.75 7.17864 0.03606 -0.00617 + 595.00 7.32396 -0.05440 -0.03341 + 595.25 7.16726 -0.42298 0.07710 + 595.50 7.30837 -0.43280 0.12859 + 595.75 7.44975 -0.50492 0.18406 + 596.00 7.45176 -0.55771 0.14265 + 596.25 7.31967 -0.80653 0.12568 + 596.50 6.85177 -0.84681 0.15034 + 596.75 6.83182 -1.14695 0.22175 + 597.00 6.92776 -0.90343 0.34831 + 597.25 7.00225 -1.00716 0.53666 + 597.50 7.03184 -0.79356 0.59447 + 597.75 7.16201 -0.72949 0.09272 + 598.00 6.91918 -0.54420 0.25336 + 598.25 6.93310 -0.44523 -0.12494 + 598.50 7.02344 -0.50669 -0.23513 + 598.75 6.79032 -0.64272 -0.63940 + 599.00 7.12034 -0.64479 -0.54164 + 599.25 7.13251 -0.72704 -0.38789 + 599.50 7.23861 -0.73126 -0.29515 + 599.75 7.25165 -0.64011 -0.20625 diff --git a/examples/FAST.Farm_interface/inputs/FFFiles/libdiscon_WT1.so b/examples/FAST.Farm_interface/inputs/FFFiles/libdiscon_WT1.so new file mode 100644 index 00000000..b95c735e Binary files /dev/null and b/examples/FAST.Farm_interface/inputs/FFFiles/libdiscon_WT1.so differ diff --git a/examples/FAST.Farm_interface/inputs/FFFiles/libdiscon_WT2.so b/examples/FAST.Farm_interface/inputs/FFFiles/libdiscon_WT2.so new file mode 100644 index 00000000..b95c735e Binary files /dev/null and b/examples/FAST.Farm_interface/inputs/FFFiles/libdiscon_WT2.so differ diff --git a/examples/FAST.Farm_interface/inputs/FFFiles/libdiscon_WT3.so b/examples/FAST.Farm_interface/inputs/FFFiles/libdiscon_WT3.so new file mode 100644 index 00000000..b95c735e Binary files /dev/null and b/examples/FAST.Farm_interface/inputs/FFFiles/libdiscon_WT3.so differ diff --git a/examples/FAST.Farm_interface/inputs/gch_whoc_example.yaml b/examples/FAST.Farm_interface/inputs/gch_whoc_example.yaml new file mode 100644 index 00000000..95090d9d --- /dev/null +++ b/examples/FAST.Farm_interface/inputs/gch_whoc_example.yaml @@ -0,0 +1,244 @@ + +### +# A name for this input file. +# This is not currently only for the user's reference. +name: GCH + +### +# A description of the contents of this input file. +# This is not currently only for the user's reference. +description: Three turbines using Gauss Curl Hybrid model + +### +# The earliest version of FLORIS this input file supports. +# This is not currently only for the user's reference. +floris_version: v4 + +### +# Configure the logging level and where to show the logs. +logging: + + ### + # Settings for logging to the console (i.e. terminal). + console: + + ### + # Can be "true" or "false". + enable: true + + ### + # Set the severity to show output. Messages at this level or higher will be shown. + # Can be one of "CRITICAL", "ERROR", "WARNING", "INFO", "DEBUG". + level: WARNING + + ### + # Settings for logging to a file. + file: + + ### + # Can be "true" or "false". + enable: false + + ### + # Set the severity to show output. Messages at this level or higher will be shown. + # Can be one of "CRITICAL", "ERROR", "WARNING", "INFO", "DEBUG". + level: WARNING + +### +# Configure the solver for the type of simulation. +solver: + + ### + # Select the solver type. + # Can be one of: "turbine_grid", "flow_field_grid", "flow_field_planar_grid". + type: turbine_grid + + ### + # Options for the turbine type selected above. See the solver documentation for available parameters. + turbine_grid_points: 3 + +### +# Configure the turbine types and their placement within the wind farm. +farm: + + ### + # Coordinates for the turbine locations in the x-direction which is typically considered + # to be the streamwise direction (left, right) when the wind is out of the west. + # The order of the coordinates here corresponds to the index of the turbine in the primary + # data structures. + layout_x: + - 0.0 + - 504.0 + - 1008.0 + + ### + # Coordinates for the turbine locations in the y-direction which is typically considered + # to be the spanwise direction (up, down) when the wind is out of the west. + # The order of the coordinates here corresponds to the index of the turbine in the primary + # data structures. + layout_y: + - 0.0 + - 0.0 + - 0.0 + + ### + # Listing of turbine types for placement at the x and y coordinates given above. + # The list length must be 1 or the same as ``layout_x`` and ``layout_y``. If it is a + # single value, all turbines are of the same type. Otherwise, the turbine type + # is mapped to the location at the same index in ``layout_x`` and ``layout_y``. + # The types can be either a name included in the turbine_library or + # a full definition of a wind turbine directly. + turbine_type: + - nrel_5MW + +### +# Configure the atmospheric conditions. +flow_field: + + ### + # Air density. + air_density: 1.225 + + ### + # The height to consider the "center" of the vertical wind speed profile + # due to shear. With a shear exponent not 1, the wind speed at this height + # will be the value given in ``wind_speeds``. Above and below this height, + # the wind speed will change according to the shear profile; see + # :py:meth:`.FlowField.initialize_velocity_field`. + # For farms consisting of one wind turbine type, use ``reference_wind_height: -1`` + # to use the hub height of the wind turbine definition. For multiple wind turbine + # types, the reference wind height must be given explicitly. + reference_wind_height: -1 + + ### + # The turbulence intensities to include in the simulation, specified as a decimal. + turbulence_intensities: + - 0.06 + + ### + # The wind directions to include in the simulation. + # 0 is north and 270 is west. + wind_directions: + - 270.0 + + ### + # The exponent used to model the wind shear profile; see + # :py:meth:`.FlowField.initialize_velocity_field`. + wind_shear: 0.12 + + ### + # The wind speeds to include in the simulation. + wind_speeds: + - 8.0 + + ### + # The wind veer as a constant value for all points in the grid. + wind_veer: 0.0 + + ### + # The conditions that are specified for use with the multi-dimensional Cp/Ct capability. + # These conditions are external to FLORIS and specified by the user. They are used internally + # through a nearest-neighbor selection process to choose the correct Cp/Ct interpolants + # to use. + multidim_conditions: + Tp: 2.5 + Hs: 3.01 + +### +# Configure the wake model. +wake: + + ### + # Select the models to use for the simulation. + # See :py:mod:`~.wake` for a list + # of available models and their descriptions. + model_strings: + + ### + # Select the wake combination model. + combination_model: sosfs + + ### + # Select the wake deflection model. + deflection_model: gauss + + ### + # Select the wake turbulence model. + turbulence_model: crespo_hernandez + + ### + # Select the wake velocity deficit model. + velocity_model: gauss + + ### + # Can be "true" or "false". + enable_secondary_steering: true + + ### + # Can be "true" or "false". + enable_yaw_added_recovery: true + + ### + # Can be "true" or "false". + enable_active_wake_mixing: false + + ### + # Can be "true" or "false". + enable_transverse_velocities: true + + ### + # Configure the parameters for the wake deflection model + # selected above. + # Additional blocks can be provided for + # models that are not enabled, but the enabled model + # must have a corresponding parameter block. + wake_deflection_parameters: + gauss: + ad: 0.0 + alpha: 0.58 + bd: 0.0 + beta: 0.077 + dm: 1.0 + ka: 0.38 + kb: 0.004 + jimenez: + ad: 0.0 + bd: 0.0 + kd: 0.05 + + ### + # Configure the parameters for the wake velocity deficit model + # selected above. + # Additional blocks can be provided for + # models that are not enabled, but the enabled model + # must have a corresponding parameter block. + wake_velocity_parameters: + cc: + a_s: 0.179367259 + b_s: 0.0118889215 + c_s1: 0.0563691592 + c_s2: 0.13290157 + a_f: 3.11 + b_f: -0.68 + c_f: 2.41 + alpha_mod: 1.0 + gauss: + alpha: 0.58 + beta: 0.077 + ka: 0.38 + kb: 0.004 + jensen: + we: 0.05 + + ### + # Configure the parameters for the wake turbulence model + # selected above. + # Additional blocks can be provided for + # models that are not enabled, but the enabled model + # must have a corresponding parameter block. + wake_turbulence_parameters: + crespo_hernandez: + initial: 0.1 + constant: 0.5 + ai: 0.8 + downstream: -0.32 diff --git a/examples/FAST.Farm_interface/inputs/hercules_input.yaml b/examples/FAST.Farm_interface/inputs/hercules_input.yaml new file mode 100644 index 00000000..91922cb0 --- /dev/null +++ b/examples/FAST.Farm_interface/inputs/hercules_input.yaml @@ -0,0 +1,25 @@ +# Name +name: lookup-based_wake_steering_FAST.Farm + +### +# Describe this emulator setup +description: FAST.Farm simulation with wake steering controller + +dt: 0.5 + +controller: + num_turbines: 2 + initial_conditions: + yaw: 270. # degrees (same for all turbines) (will this work?) + +plant: + n_turbines: 3 + +emulator: + port : 5556 + timeout: 120.0 + verbose: true + logfile: log.txt + simtype: FAST.Farm # FAST.Farm or amr-wind + siminput: inputs/FFFiles/FFarm_mod.fstf + simexe: /home/abhineet/MySoftware/MicroMamba/envs/MySci/bin/FAST.Farm diff --git a/hycon/interfaces/rosco_zmq_interface.py b/hycon/interfaces/rosco_zmq_interface.py index 856d2b00..215820e2 100644 --- a/hycon/interfaces/rosco_zmq_interface.py +++ b/hycon/interfaces/rosco_zmq_interface.py @@ -1,161 +1,108 @@ -import zmq +import multiprocessing as mp +import subprocess -from hycon.interfaces.interface_base import InterfaceBase +from rosco.toolbox.control_interface import wfc_zmq_server -# Code copied from ROSCO; consider just importing and using that code -# directly?? +from hycon.interfaces.interface_base import InterfaceBase class ROSCO_ZMQInterface(InterfaceBase): - def __init__( - self, network_address="tcp://*:5555", identifier="0", timeout=600.0, verbose=False - ): - """Python implementation of the ZeroMQ server side for the ROSCO - ZeroMQ wind farm control interface. This class makes it easy for - users to receive measurements from ROSCO and then send back control - setpoints (generator torque, nacelle heading and/or blade pitch - angles). - Args: - network_address (str, optional): The network address to - communicate over with the desired instance of ROSCO. Note that, - if running a wind farm simulation in SOWFA or FAST.Farm, there - are multiple instances of ROSCO and each of these instances - needs to communicate over a unique port. Also, for each of those - instances, you will need an instance of zmq_server. Defaults to - "tcp://*:5555". - identifier (str, optional): Turbine identifier. Defaults to "0". - timeout (float, optional): Seconds to wait for a message from - the ZeroMQ server before timing out. Defaults to 600.0. - verbose (bool, optional): Print to console. Defaults to False. - """ + def __init__(self, h_dict): super().__init__() - self.network_address = network_address - self.identifier = identifier - self.timeout = timeout - self.verbose = verbose - self._connect() - - def _connect(self): - """ - Connect to zmq server - """ - address = self.network_address - - # Connect socket - context = zmq.Context() - self.socket = context.socket(zmq.REP) - self.socket.setsockopt(zmq.LINGER, 0) - self.socket.bind(address) - - if self.verbose: - print("[%s] Successfully established connection with %s" % (self.identifier, address)) - - def _disconnect(self): - """ - Disconnect from zmq server - """ - self.socket.close() - context = zmq.Context() - context.term() - - def get_measurements(self, _): - """ - Receive measurements from ROSCO .dll - """ - if self.verbose: - print("[%s] Waiting to receive measurements from ROSCO..." % (self.identifier)) - - # Initialize a poller for timeouts - poller = zmq.Poller() - poller.register(self.socket, zmq.POLLIN) - timeout_ms = int(self.timeout * 1000) - if poller.poll(timeout_ms): - # Receive measurements over network protocol - message_in = self.socket.recv_string() + # Controller parameters + if "controller" in h_dict and h_dict["controller"] is not None: + self.controller_parameters = h_dict["controller"] else: - raise IOError( - "[%s] Connection to '%s' timed out." % (self.identifier, self.network_address) - ) - - # Convert to individual strings and then to floats - measurements = message_in - measurements = measurements.replace("\x00", "").split(",") - measurements = [float(m) for m in measurements] - - # Convert to a measurement dict - measurements = dict( - { - "Turbine_ID": measurements[0], - "iStatus": measurements[1], - "Time": measurements[2], - "VS_MechGenPwr": measurements[3], - "VS_GenPwr": measurements[4], - "GenSpeed": measurements[5], - "RotSpeed": measurements[6], - "GenTqMeas": measurements[7], - "NacelleHeading": measurements[8], - "NacelleVane": measurements[9], - "HorWindV": measurements[10], - "rootMOOP1": measurements[11], - "rootMOOP2": measurements[12], - "rootMOOP3": measurements[13], - "FA_Acc": measurements[14], - "NacIMU_FA_Acc": measurements[15], - "Azimuth": measurements[16], - } - ) - - if self.verbose: - print("[%s] Measurements received:" % self.identifier, measurements) - - return measurements - - def check_controls(self, controls_dict): - available_controls = [ - "turbine_ID", - "genTorque", - "nacelleHeading", - "bladePitch", - ] + self.controller_parameters = {} + + # Plant parameters + if "plant" in h_dict and h_dict["plant"] is not None: + self.plant_parameters = h_dict["plant"] + else: + self.plant_parameters = {} + + # Emulator parameters + if "emulator" in h_dict and h_dict["emulator"] is not None: + self.emulator_parameters = h_dict["emulator"] + else: + self.emulator_parameters = {} + + def get_measurements(self): + pass - for k in controls_dict.keys(): - if k not in available_controls: - raise ValueError("Setpoint " + k + " is not available in this configuration") + def check_controls(self): + pass + + # def addcontroller(self, controller): + # self.controller = controller def send_controls( self, turbine_ID=0, genTorque=0.0, nacelleHeading=0.0, bladePitch=[0.0, 0.0, 0.0] ): - """ - Send controls to ROSCO .dll ffor individual turbine control - - Parameters: - ----------- - genTorques: float - Generator torque setpoint - nacelleHeadings: float - Nacelle heading setpoint - bladePitchAngles: List (len=3) - Blade pitch angle setpoint - """ - # Create a message with controls to send to ROSCO - message_out = b"%016.5f, %016.5f, %016.5f, %016.5f, %016.5f, %016.5f" % ( - turbine_ID, - genTorque, - nacelleHeading, - bladePitch[0], - bladePitch[1], - bladePitch[2], - ) - - # Send reply back to client - if self.verbose: - print("[%s] Sending setpoint string to ROSCO: %s." % (self.identifier, message_out)) - - # Send control controls over network protocol - self.socket.send(message_out) - - if self.verbose: - print("[%s] Setpoints sent successfully." % self.identifier) - - return None + pass + + +class ROSCO_Emulator: + def __init__(self, interface, controller): + self.interface = interface + self.controller = controller + + def startserverandsim(self): + pserver = mp.Process(target=self.run_zmq, args=()) + psim = mp.Process(target=self.rumfarmsim, args=()) + + pserver.start() + psim.start() + + psim.join() + pserver.join() + + def run_zmq(self): + """Start the ZeroMQ server for wind farm control""" + # Start the server at the following address + + network_address = f"tcp://*:{self.interface.emulator_parameters['port']}" + server = wfc_zmq_server(network_address, timeout=60.0, verbose=False, logfile="log.txt") + + # Provide the wind farm control algorithm as the wfc_controller method of the server + i_wfc_cont = intermediate_wfc_controller(self.interface, self.controller) + server.wfc_controller = i_wfc_cont + + # Run the server to receive measurements and send setpoints + server.runserver() + + def rumfarmsim(self): + simexe = self.interface.emulator_parameters["simexe"] + siminput = self.interface.emulator_parameters["siminput"] + simcmd = f"{simexe} {siminput}" + print(f"Running simulation with command '{simcmd}'") + subprocess.run(simcmd, shell=True, check=True) + + +class intermediate_wfc_controller: + def __init__(self, interface, controller): + self.interface = interface + self.controller = controller + self.n_turbines = self.interface.plant_parameters["n_turbines"] + self.measurements_to_hycon_controller = {k: 0 for k in range(self.n_turbines)} + self.controls_from_hycon_controller = {} + + def update_setpoints(self, id, current_time, measurements): + if len(self.measurements_to_hycon_controller) == self.n_turbines: + self.controls_from_hycon_controller = self.getcontrolsfromhycon() + self.measurements_to_hycon_controller = {} + + self.measurements_to_hycon_controller[id] = measurements["NacVane"] + + setpoints = {} + setpoints["ZMQ_YawOffset"] = self.controls_from_hycon_controller[id] + return setpoints + + def getcontrolsfromhycon(self): + measurements_dict = {} + measurements_dict["wind_farm"] = {} + measurements_dict["wind_farm"]["wind_directions"] = [ + self.measurements_to_hycon_controller[i] for i in range(self.n_turbines) + ] + self.controller.compute_controls(measurements_dict) diff --git a/pyproject.toml b/pyproject.toml index 2b25e448..821ec04d 100644 --- a/pyproject.toml +++ b/pyproject.toml @@ -28,6 +28,7 @@ dependencies = [ "matplotlib~=3.0", "floris~=4.3", "zmq", + "rosco~=2.10", ] [project.optional-dependencies]