diff options
Diffstat (limited to 'example_airfoil.py')
| -rw-r--r-- | example_airfoil.py | 29 |
1 files changed, 15 insertions, 14 deletions
diff --git a/example_airfoil.py b/example_airfoil.py index 0fd0aba..e0eb532 100644 --- a/example_airfoil.py +++ b/example_airfoil.py @@ -10,26 +10,27 @@ Generate a population of airfoils & optimize. from tools import creator, evaluator, generator + import time start_time = time.time() -# Airfoil dimensions +# Airfoil dimensions (in) NACA_NUM = 2412 -CHORD_LENGTH = 68 # inches -SEMI_SPAN = 150 # inches +CHORD_LENGTH = 68 +SEMI_SPAN = 150 # Thicknesses SPAR_THICKNESS = 0.4 SKIN_THICKNESS = 0.1 -# Component masses -AIRFOIL_MASS = 10 # lbs -SPAR_MASS = 10 # lbs -STRINGER_MASS = 5 # lbs +# Component masses (lbs) +AIRFOIL_MASS = 10 +SPAR_MASS = 10 +STRINGER_MASS = 5 -# Area -SPAR_CAP_AREA = 0.3 # sqin -STRINGER_AREA = 0.1 # sqin +# Area (sqin) +SPAR_CAP_AREA = 0.3 +STRINGER_AREA = 0.1 # Amount of stringers TOP_STRINGERS = 6 @@ -37,7 +38,7 @@ BOTTOM_STRINGERS = 4 NOSE_TOP_STRINGERS = 3 NOSE_BOTTOM_STRINGERS = 5 -SAVE_PATH = 'C:/Users/blend/github/UCLA_MAE_154B/save' +SAVE_PATH = '/home/blendux/github/UCLA_MAE_154B/save/' # Create airfoil instance @@ -87,9 +88,9 @@ evaluator.plot_lift(eval) pop = generator.Population(10) -print(help(creator)) -print(help(evaluator)) -print(help(generator)) +# print(help(creator)) +# print(help(evaluator)) +# print(help(generator)) # Print final execution time print("--- %s seconds ---" % (time.time() - start_time)) |