diff options
Diffstat (limited to 'main.py')
| -rw-r--r-- | main.py | 22 |
1 files changed, 11 insertions, 11 deletions
@@ -66,20 +66,20 @@ def main(): # 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() # Define the spar coordinates and mass, stored in single spar object af.spar.add_coord(af, 0.23) af.spar.add_coord(af, 0.57) - # Automatically adds spar caps for every previously defined + # Automatically adds spar caps for each spar defined previously 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() @@ -92,24 +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, True) # 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) pop = generator.Population(10) - print(help(creator)) + # print(help(creator)) # print(help(evaluator)) # print(help(generator)) |