diff options
Diffstat (limited to 'main.py')
| -rw-r--r-- | main.py | 12 |
1 files changed, 6 insertions, 6 deletions
@@ -56,7 +56,7 @@ def main(): # Define NACA airfoil coordinates and mass af.add_naca(2412) af.add_mass(AIRFOIL_MASS) - # af.print_info(2) + af.print_info(2) # Create spar instance af.spar = creator.Spar() @@ -64,7 +64,7 @@ def main(): af.spar.add_coord(af.coord, 0.15) af.spar.add_coord(af.coord, 0.55) af.spar.add_mass(SPAR_MASS) - # af.spar.print_info(2) + af.spar.print_info(2) # Create stringer instance af.stringer = creator.Stringer() @@ -75,12 +75,12 @@ def main(): af.stringer.print_info(2) # Plot components with matplotlib - # creator.plot(af, af.spar, af.stringer) + creator.plot(af, af.spar, af.stringer) # Save component info - # af.save_info(SAVE_PATH, _) - # af.spar.save_info(SAVE_PATH, _) - # af.stringer.save_info(SAVE_PATH, _) + af.save_info(SAVE_PATH, _) + af.spar.save_info(SAVE_PATH, _) + af.stringer.save_info(SAVE_PATH, _) # Evaluate previously created airfoil(s). total_mass = evaluator.get_total_mass(af, af.spar, af.stringer) |