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author | Marius Peter <blendoit@gmail.com> | 2019-06-24 19:10:41 -0700 |
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committer | Marius Peter <blendoit@gmail.com> | 2019-06-24 19:10:41 -0700 |
commit | 576c9232ec279b6f9e50f7c4d56c9836208d1c07 (patch) | |
tree | 2ed84801a6857b24107a3d1c68d218094ef0c6f5 /main.py | |
parent | d9e01e38d69111c71308b19bb60d315187f312d9 (diff) |
variable name consistency & docstrings
Diffstat (limited to 'main.py')
-rw-r--r-- | main.py | 8 |
1 files changed, 4 insertions, 4 deletions
@@ -25,7 +25,7 @@ start_time = time.time() # Airfoil dimensions NACA_NUM = 2412 CHORD_LENGTH = 68 # inches -SEMI_SPAN = 100 # inches +SEMI_SPAN = 150 # inches # Airfoil thickness T_UPPER = 0.1 @@ -44,7 +44,7 @@ STRINGER_AREA = 0.1 # sqin TOP_STRINGERS = 6 BOTTOM_STRINGERS = 4 NOSE_TOP_STRINGERS = 3 -NOSE_BOTTOM_STRINGERS = 6 +NOSE_BOTTOM_STRINGERS = 5 # population information & save path POP_SIZE = 1 @@ -98,7 +98,7 @@ def main(): af.stringer.info_save(SAVE_PATH, _) # Plot components with matplotlib - creator.plot_geom(af) + # creator.plot_geom(af) # Evaluator object contains airfoil analysis results. eval = evaluator.Evaluator(af) @@ -106,7 +106,7 @@ def main(): eval.analysis() # eval.info_print(2) eval.info_save(SAVE_PATH, _) - # evaluator.plot_geom(eval) + evaluator.plot_geom(eval) # evaluator.plot_lift(eval) # Print final execution time |