diff options
Diffstat (limited to 'main.py')
-rw-r--r-- | main.py | 18 |
1 files changed, 9 insertions, 9 deletions
@@ -23,9 +23,9 @@ import time start_time = time.time() # Airfoil dimensions -NACA_NUM = 4412 -CHORD_LENGTH = 133 -SEMI_SPAN = 140 +NACA_NUM = 2412 +CHORD_LENGTH = 101 +SEMI_SPAN = 40 # Airfoil thickness T_UPPER = 0.1 @@ -37,11 +37,11 @@ SPAR_MASS = 10 # lbs STRINGER_MASS = 5 # lbs # Area -SPAR_CAP_AREA = 0.3 # sqin +SPAR_CAP_AREA = 0.0 # sqin STRINGER_AREA = 0.1 # sqin # Amount of stringers -TOP_STRINGERS = 5 +TOP_STRINGERS = 3 BOTTOM_STRINGERS = 4 NOSE_TOP_STRINGERS = 3 NOSE_BOTTOM_STRINGERS = 6 @@ -71,7 +71,7 @@ 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() @@ -82,7 +82,7 @@ def main(): af.spar.add_spar_caps(SPAR_CAP_AREA) af.spar.add_mass(SPAR_MASS) # af.spar.info_print(2) - # af.spar.info_save(SAVE_PATH, _) + af.spar.info_save(SAVE_PATH, _) # Create stringer instance af.stringer = creator.Stringer() @@ -95,7 +95,7 @@ def main(): af.stringer.add_area(STRINGER_AREA) af.stringer.add_mass(STRINGER_MASS) # 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) @@ -106,7 +106,7 @@ def main(): eval.analysis() # eval.info_print(2) eval.info_save(SAVE_PATH, _) - evaluator.plot_geom(eval) + # evaluator.plot_geom(eval) # evaluator.plot_lift(eval) # Print final execution time |