diff options
Diffstat (limited to 'main.py')
-rw-r--r-- | main.py | 16 |
1 files changed, 8 insertions, 8 deletions
@@ -58,8 +58,8 @@ def main(): # Define NACA airfoil coordinates and mass af.add_naca(NACA_NUM) af.add_mass(AIRFOIL_MASS) - # af.print_info(2) - # af.save_info(SAVE_PATH, _) + # af.info_print(2) + # af.info_save(SAVE_PATH, _) # Create spar instance af.spar = creator.Spar() @@ -67,8 +67,8 @@ 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.save_info(SAVE_PATH, _) + # af.spar.info_print(2) + # af.spar.info_save(SAVE_PATH, _) # Create stringer instance af.stringer = creator.Stringer() @@ -76,8 +76,8 @@ def main(): af.stringer.add_coord(af.coord, af.spar.coord, 4, 7, 5, 6) af.stringer.add_area(STRINGER_AREA) af.stringer.add_mass(STRINGER_MASS) - # af.stringer.print_info(2) - # af.stringer.save_info(SAVE_PATH, _) + # af.stringer.info_print(2) + # af.stringer.info_save(SAVE_PATH, _) # Plot components with matplotlib # af.plot() @@ -86,8 +86,8 @@ def main(): eval = evaluator.Airfoil(af) # The analysis is performed in the evaluator.py module. eval.analysis() - eval.print_info(2) - # eval.save_info(SAVE_PATH, _) + eval.info_print(2) + # eval.info_save(SAVE_PATH, _) # eval.plot() # Print final execution time |