Merge remote-tracking branch 'origin/develop' into develop

Author: peterdsharpe

README.md

@@ -268,7 +268,7 @@ For more details, see the [changelog](./CHANGELOG.md).
 
 ### Citation & Commercial Use
 
-If you find AeroSandbox useful in a research publication, please cite one of the following publications:
+If you find AeroSandbox useful in a research publication, please cite the following publications:
 
 [The author's PhD thesis](./tutorial/sharpe-pds-phd-AeroAstro-2024-thesis.pdf):
 
@@ -303,3 +303,7 @@ If you use AeroSandbox, attribution is appreciated.
 ## Stargazers over time
 
 [![Stargazers over time](https://starchart.cc/peterdsharpe/AeroSandbox.svg)](https://starchart.cc/peterdsharpe/AeroSandbox) 
+
+## Supported by
+
+<a href="https://jb.gg/OpenSourceSupport"><img src="https://resources.jetbrains.com/storage/products/company/brand/logos/jetbrains.svg" alt="JetBrains logo."></a>

aerosandbox/aerodynamics/aero_3D/avl.py

@@ -1,12 +1,13 @@
-from aerosandbox.common import ExplicitAnalysis
-import aerosandbox.numpy as np
 import subprocess
-from pathlib import Path
-from aerosandbox.geometry import Airplane, Wing, WingXSec, Fuselage, ControlSurface
-from aerosandbox.performance import OperatingPoint
-from typing import Union, List, Dict
 import tempfile
 import warnings
+from pathlib import Path
+from typing import Dict, List, Union
+
+import aerosandbox.numpy as np
+from aerosandbox.common import ExplicitAnalysis
+from aerosandbox.geometry import Airplane, ControlSurface, Fuselage, Wing, WingXSec
+from aerosandbox.performance import OperatingPoint
 
 
 class AVL(ExplicitAnalysis):
@@ -341,7 +342,6 @@ def run(
             return res
 
     def _default_keystroke_file_contents(self) -> List[str]:
-
         run_file_contents = []
 
         # Disable graphics
@@ -441,7 +441,6 @@ def clean(s):
         airfoil_counter = 0
 
         for wing in airplane.wings:
-
             wing_options = self.get_options(wing)
 
             spacing_line = f"{wing_options['chordwise_resolution']}   {self.AVL_spacing_parameters[wing_options['chordwise_spacing']]}"
@@ -533,7 +532,6 @@ def clean(s):
 
             ### Write the commands for each wing section
             for i, xsec in enumerate(wing.xsecs):
-
                 xsec_options = self.get_options(xsec)
 
                 xsec_def_line = f"{xsec.xyz_le[0]:.8g} {xsec.xyz_le[1]:.8g} {xsec.xyz_le[2]:.8g} {xsec.chord:.8g} {xsec.twist:.8g}"
@@ -743,7 +741,6 @@ def parse_unformatted_data_output(
         index = s.find(data_identifier)
 
         while index != -1:  # While there are still data identifiers:
-
             key = ""  # start with a blank key, which we will build up as we read
 
             i = index - 1  # Starting from the left of the identifier
@@ -804,10 +801,8 @@ def parse_unformatted_data_output(
 
 
 if __name__ == "__main__":
-
     ### Import Vanilla Airplane
     import aerosandbox as asb
-
     from aerosandbox.aerodynamics.aero_3D.test_aero_3D.geometries.vanilla import (
         airplane as vanilla,
     )