diff options
Diffstat (limited to 'main.py')
| -rw-r--r-- | main.py | 14 |
1 files changed, 7 insertions, 7 deletions
@@ -70,7 +70,7 @@ def main(): # Define NACA airfoil coordinates and mass af.add_naca(NACA_NUM) af.add_mass(AIRFOIL_MASS) - # af.info_print(2) + af.info_print(2) af.info_save(SAVE_PATH, _) # Create spar instance @@ -82,7 +82,7 @@ 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_print(2) af.spar.info_save(SAVE_PATH, _) # Create stringer instance @@ -96,20 +96,20 @@ 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_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() - # eval.info_print(2) + eval.analysis(1, 1) + eval.info_print(2) eval.info_save(SAVE_PATH, _) evaluator.plot_geom(eval) - # evaluator.plot_lift(eval) + evaluator.plot_lift(eval) # Print final execution time print("--- %s seconds ---" % (time.time() - start_time)) |