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incompressible_flow/Inc_Heated_Cylinders/mesh_cht_3cyl.su2
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incompressible_flow/Inc_Streamwise_Periodic/chtPinArray_2d.geo
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incompressible_flow/Inc_Streamwise_Periodic/fluid_FFD.su2
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incompressible_flow/Inc_Streamwise_Periodic/sp_pinArray_2d_dp_hf_tp.cfg
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%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%% | ||
% % | ||
% SU2 configuration file % | ||
% Case description: Unit Cell flow around pin array (fluid) % | ||
% Author: T. Kattmann % | ||
% Institution: Robert Bosch GmbH % | ||
% Date: 2020.12.15 % | ||
% % | ||
%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%% | ||
% | ||
% ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------% | ||
% | ||
SOLVER= INC_RANS | ||
KIND_TURB_MODEL= SST | ||
% | ||
% ---------------- INCOMPRESSIBLE FLOW CONDITION DEFINITION -------------------% | ||
% | ||
INC_DENSITY_MODEL= CONSTANT | ||
INC_DENSITY_INIT= 1045.0 | ||
INC_VELOCITY_INIT= ( 0.1, 0.0, 0.0 ) | ||
% | ||
INC_ENERGY_EQUATION = YES | ||
INC_TEMPERATURE_INIT= 338.0 | ||
INC_NONDIM= DIMENSIONAL | ||
SPECIFIC_HEAT_CP= 3540.0 | ||
% | ||
FREESTREAM_TURBULENCEINTENSITY= 0.05 | ||
FREESTREAM_TURB2LAMVISCRATIO= 10.0 | ||
% | ||
% --------------------------- VISCOSITY MODEL ---------------------------------% | ||
% | ||
VISCOSITY_MODEL= CONSTANT_VISCOSITY | ||
MU_CONSTANT= 0.001385 | ||
% | ||
% --------------------------- THERMAL CONDUCTIVITY MODEL ----------------------% | ||
% | ||
% Pr_lam = mu_lam [Pa*s] * c_p [J/(kg*K)] / lambda[W/(m*K)] | ||
% = 1.385e-3 * 3540 / 0.42 | ||
% = 11.7 | ||
CONDUCTIVITY_MODEL= CONSTANT_PRANDTL | ||
PRANDTL_LAM= 11.7 | ||
% | ||
TURBULENT_CONDUCTIVITY_MODEL= CONSTANT_PRANDTL_TURB | ||
PRANDTL_TURB= 0.90 | ||
% | ||
% --------------------- STREAMWISE PERIODICITY DEFINITION ---------------------% | ||
% | ||
KIND_STREAMWISE_PERIODIC= PRESSURE_DROP | ||
STREAMWISE_PERIODIC_PRESSURE_DROP= 208.023676 | ||
% | ||
STREAMWISE_PERIODIC_TEMPERATURE= YES | ||
% | ||
% -------------------- BOUNDARY CONDITION DEFINITION --------------------------% | ||
% | ||
MARKER_HEATFLUX= ( fluid_pin1_interface, 5e5, \ | ||
fluid_pin2_interface, 5e5, \ | ||
fluid_pin3_interface, 5e5 ) | ||
MARKER_SYM= ( fluid_symmetry ) | ||
MARKER_PERIODIC= ( fluid_inlet, fluid_outlet, 0.0,0.0,0.0, 0.0,0.0,0.0, 0.0111544,0.0,0.0 ) | ||
% | ||
% Alternative to periodic simulation with velocity inlet and pressure outlet | ||
%INC_INLET_TYPE= VELOCITY_INLET | ||
%MARKER_INLET= ( fluid_inlet, 338.0, 0.75, 1.0, 0.0, 0.0 ) | ||
%INC_OUTLET_TYPE= PRESSURE_OUTLET | ||
%MARKER_OUTLET= ( fluid_outlet, 0.0 ) | ||
% | ||
% ------------------------ SURFACES IDENTIFICATION ----------------------------% | ||
% | ||
MARKER_MONITORING= ( fluid_pin2_interface ) | ||
% | ||
MARKER_ANALYZE = ( fluid_outlet, fluid_inlet ) | ||
MARKER_ANALYZE_AVERAGE = MASSFLUX | ||
% | ||
% ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------% | ||
% | ||
ITER= 3500 | ||
NUM_METHOD_GRAD= GREEN_GAUSS | ||
CFL_NUMBER= 1e2 | ||
% | ||
% ------------------------ LINEAR SOLVER DEFINITION ---------------------------% | ||
% | ||
LINEAR_SOLVER= FGMRES | ||
LINEAR_SOLVER_PREC= ILU | ||
LINEAR_SOLVER_ERROR= 1e-3 | ||
LINEAR_SOLVER_ITER= 20 | ||
% | ||
% -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------% | ||
% | ||
CONV_NUM_METHOD_FLOW= FDS | ||
MUSCL_FLOW= YES | ||
SLOPE_LIMITER_FLOW= NONE | ||
% | ||
TIME_DISCRE_FLOW= EULER_IMPLICIT | ||
% | ||
% -------------------- TURBULENT NUMERICAL METHOD DEFINITION ------------------% | ||
% | ||
CONV_NUM_METHOD_TURB= SCALAR_UPWIND | ||
MUSCL_TURB= NO | ||
SLOPE_LIMITER_TURB= NONE | ||
% | ||
TIME_DISCRE_TURB= EULER_IMPLICIT | ||
% | ||
% --------------------------- CONVERGENCE PARAMETERS --------------------------% | ||
% | ||
CONV_CRITERIA= RESIDUAL | ||
CONV_FIELD= RMS_TEMPERATURE | ||
CONV_RESIDUAL_MINVAL= -4.07 | ||
CONV_STARTITER= 10 | ||
% | ||
% ------------------------- INPUT/OUTPUT INFORMATION --------------------------% | ||
% | ||
MESH_FILENAME= fluid_FFD.su2 | ||
% | ||
SCREEN_OUTPUT= (INNER_ITER, RMS_PRESSURE, RMS_TEMPERATURE, STREAMWISE_MASSFLOW, STREAMWISE_DP) | ||
SCREEN_WRT_FREQ_INNER= 100 | ||
% | ||
HISTORY_OUTPUT= ( ITER, RMS_RES, STREAMWISE_PERIODIC, FLOW_COEFF, LINSOL, AERO_COEFF ) | ||
CONV_FILENAME= history_dptp | ||
% | ||
OUTPUT_FILES= ( RESTART, PARAVIEW_MULTIBLOCK ) | ||
VOLUME_OUTPUT= ( COORDINATES, SOLUTION, RESIDUAL, PRIMITIVE ) | ||
OUTPUT_WRT_FREQ= 5000 | ||
% | ||
% -------------------- FREE-FORM DEFORMATION PARAMETERS -----------------------% | ||
% | ||
FFD_TOLERANCE= 1E-10 | ||
FFD_ITERATIONS= 500 | ||
% | ||
% FFD box definition: 2D case (FFD_BoxTag, X1, Y1, 0.0, X2, Y2, 0.0, X3, Y3, 0.0, X4, Y4, 0.0, | ||
% 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0) | ||
FFD_DEFINITION= (BOX, 0.0029772,0.0,0.0, 0.0081772,0.0,0.0 0.0081772,0.0026,0.0, 0.0029772,0.0026,0.0, 0.0,0.0,0.0, 0.0,0.0,0.0 0.0,0.0,0.0, 0.0,0.0,0.0 ) | ||
% | ||
% FFD box degree: 2D case (x_degree, y_degree, 0) | ||
FFD_DEGREE= (8, 1, 0) | ||
% | ||
% Surface grid continuity at the intersection with the faces of the FFD boxes. | ||
% To keep a particular level of surface continuity, SU2 automatically freezes the right | ||
% number of control point planes (NO_DERIVATIVE, 1ST_DERIVATIVE, 2ND_DERIVATIVE, USER_INPUT) | ||
FFD_CONTINUITY= NO_DERIVATIVE | ||
% | ||
% ----------------------- DESIGN VARIABLE PARAMETERS --------------------------% | ||
% | ||
DV_KIND= FFD_SETTING | ||
%DV_KIND= FFD_CONTROL_POINT_2D,FFD_CONTROL_POINT_2D,FFD_CONTROL_POINT_2D,FFD_CONTROL_POINT_2D,FFD_CONTROL_POINT_2D,FFD_CONTROL_POINT_2D,FFD_CONTROL_POINT_2D,FFD_CONTROL_POINT_2D,FFD_CONTROL_POINT_2D | ||
% | ||
% Marker of the surface in which we are going apply the shape deformation | ||
DV_MARKER= ( fluid_pin2_interface ) | ||
% | ||
% Parameters of the shape deformation | ||
% - FFD_SETTING ( 1.0 ) | ||
% - FFD_CONTROL_POINT_2D ( FFD_BoxTag, i_Ind, j_Ind, x_Disp, y_Disp ) | ||
DV_PARAM= ( 1.0 ) | ||
%DV_PARAM= \ | ||
%( BOX, 0, 1, 0.0, 1.0);\ | ||
%( BOX, 1, 1, 0.0, 1.0);\ | ||
%( BOX, 2, 1, 0.0, 1.0);\ | ||
%( BOX, 3, 1, 0.0, 1.0);\ | ||
%( BOX, 4, 1, 0.0, 1.0);\ | ||
%( BOX, 5, 1, 0.0, 1.0);\ | ||
%( BOX, 6, 1, 0.0, 1.0);\ | ||
%( BOX, 7, 1, 0.0, 1.0);\ | ||
%( BOX, 8, 1, 0.0, 1.0) | ||
% | ||
% Value of the shape deformation | ||
DV_VALUE= 1.0 | ||
%DV_VALUE= 1.0,1.0,1.0,1.0,1.0,1.0,1.0,1.0,1.0,1.0,1.0,1.0,1.0,1.0,1.0,1.0,1.0,1.0 | ||
% | ||
% ------------------------ GRID DEFORMATION PARAMETERS ------------------------% | ||
% | ||
DEFORM_LINEAR_SOLVER= FGMRES | ||
DEFORM_LINEAR_SOLVER_PREC= ILU | ||
DEFORM_LINEAR_SOLVER_ERROR= 1E-14 | ||
DEFORM_NONLINEAR_ITER= 1 | ||
DEFORM_LINEAR_SOLVER_ITER= 1000 | ||
% | ||
DEFORM_CONSOLE_OUTPUT= YES | ||
DEFORM_STIFFNESS_TYPE= WALL_DISTANCE | ||
% | ||
% Deformation coefficient (linear elasticity limits from -1.0 to 0.5, a larger | ||
% value is also possible) | ||
% !!! What is this doing !!! | ||
DEFORM_COEFF = 1E6 | ||
% | ||
DEFINITION_DV= \ | ||
( 19, 1.0 | fluid_pin2_interface | BOX, 0, 1, 0.0, 1.0 ); \ | ||
( 19, 1.0 | fluid_pin2_interface | BOX, 1, 1, 0.0, 1.0 ); \ | ||
( 19, 1.0 | fluid_pin2_interface | BOX, 2, 1, 0.0, 1.0 ); \ | ||
( 19, 1.0 | fluid_pin2_interface | BOX, 3, 1, 0.0, 1.0 ); \ | ||
( 19, 1.0 | fluid_pin2_interface | BOX, 4, 1, 0.0, 1.0 ); \ | ||
( 19, 1.0 | fluid_pin2_interface | BOX, 5, 1, 0.0, 1.0 ); \ | ||
( 19, 1.0 | fluid_pin2_interface | BOX, 6, 1, 0.0, 1.0 ); \ | ||
( 19, 1.0 | fluid_pin2_interface | BOX, 7, 1, 0.0, 1.0 ); \ | ||
( 19, 1.0 | fluid_pin2_interface | BOX, 8, 1, 0.0, 1.0 ) | ||
%DEFORM_MESH= YES | ||
% | ||
% Finite difference step size for python scripts (0.001 default, recommended | ||
% 0.001 x REF_LENGTH) | ||
FIN_DIFF_STEP= 1e-6 |
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