diff options
Diffstat (limited to 'main.py')
| -rw-r--r-- | main.py | 27 |
1 files changed, 12 insertions, 15 deletions
@@ -57,20 +57,17 @@ def main(): Evaluate an airfoil; Generate a population of airfoils & optimize. """ - # Create coordinate system specific to our airfoil dimensions. - # TODO: imperial + metric unit setting - creator.Coordinates(CHORD_LENGTH, SEMI_SPAN) # Interate through all wings in population, creating and evaluating them. for _ in range(1, POP_SIZE + 1): # Create airfoil instance - af = creator.Airfoil() + af = creator.Airfoil.from_dimensions(CHORD_LENGTH, SEMI_SPAN) # Define NACA airfoil coordinates and mass af.add_naca(NACA_NUM) af.add_mass(AIRFOIL_MASS) - # af.info_print(2) - # af.info_save(SAVE_PATH, _) + af.info_print(2) + af.info_save(SAVE_PATH, _) # Create spar instance af.spar = creator.Spar() @@ -81,8 +78,8 @@ def main(): af.spar.add_spar_caps(SPAR_CAP_AREA) af.spar.add_mass(SPAR_MASS) af.spar.add_webs(SPAR_THICKNESS) - # af.spar.info_print(2) - # af.spar.info_save(SAVE_PATH, _) + af.spar.info_print(2) + af.spar.info_save(SAVE_PATH, _) # Create stringer instance af.stringer = creator.Stringer() @@ -95,24 +92,24 @@ def main(): af.stringer.add_area(STRINGER_AREA) af.stringer.add_mass(STRINGER_MASS) af.stringer.add_webs(SKIN_THICKNESS) - # af.stringer.info_print(2) - # af.stringer.info_save(SAVE_PATH, _) + af.stringer.info_print(2) + 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) # The analysis is performed in the evaluator.py module. eval.analysis(1, 1) - # eval.info_print(2) - # eval.info_save(SAVE_PATH, _) + eval.info_print(2) + eval.info_save(SAVE_PATH, _) evaluator.plot_geom(eval) - # evaluator.plot_lift(eval) + evaluator.plot_lift(eval) pop = generator.Population(10) - # print(help(creator)) + print(help(creator)) # print(help(evaluator)) # print(help(generator)) |