diff options
Diffstat (limited to 'main.py')
| -rw-r--r-- | main.py | 12 |
1 files changed, 6 insertions, 6 deletions
@@ -24,7 +24,7 @@ start_time = time.time() # Airfoil dimensions NACA_NUM = 2412 -CHORD_LENGTH = 68 # inches +CHORD_LENGTH = 2 # inches SEMI_SPAN = 150 # inches # Thicknesses @@ -67,7 +67,7 @@ def main(): af.add_naca(NACA_NUM) af.add_mass(AIRFOIL_MASS) # af.info_print(2) - # af.info_save(SAVE_PATH, _) + af.info_save(SAVE_PATH, _) # Create spar instance af.spar = creator.Spar() @@ -79,7 +79,7 @@ def main(): 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_save(SAVE_PATH, _) # Create stringer instance af.stringer = creator.Stringer() @@ -93,17 +93,17 @@ def main(): 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_save(SAVE_PATH, _) # Plot components with matplotlib - creator.plot_geom(af, True) + # 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_save(SAVE_PATH, _) # evaluator.plot_geom(eval) # evaluator.plot_lift(eval) |