From 3074c4c8cbeac6a6e5a4d7fa4a8afe34ec39911d Mon Sep 17 00:00:00 2001 From: Marius Peter Date: Sun, 23 Jun 2019 02:09:34 -0700 Subject: finalised branch :) --- main.py | 20 ++++++++++---------- 1 file changed, 10 insertions(+), 10 deletions(-) (limited to 'main.py') diff --git a/main.py b/main.py index 2f1ba1f..b62b24f 100644 --- a/main.py +++ b/main.py @@ -25,7 +25,7 @@ start_time = time.time() # Airfoil dimensions NACA_NUM = 2412 CHORD_LENGTH = 100 -SEMI_SPAN = 20 +SEMI_SPAN = 140 # Airfoil thickness T_UPPER = 0.1 @@ -41,8 +41,8 @@ SPAR_CAP_AREA = 0.3 # sqin STRINGER_AREA = 0.1 # sqin # Amount of stringers -TOP_STRINGERS = 4 -BOTTOM_STRINGERS = 7 +TOP_STRINGERS = 5 +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() @@ -95,17 +95,17 @@ 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) + # creator.plot_geom(af) # Evaluator object contains airfoil analysis results. - # eval = evaluator.Evaluator(af) + eval = evaluator.Evaluator(af) # The analysis is performed in the evaluator.py module. - # eval.analysis() + eval.analysis() # eval.info_print(2) - # eval.info_save(SAVE_PATH, _) + eval.info_save(SAVE_PATH, _) # evaluator.plot_geom(eval) # evaluator.plot_lift(eval) -- cgit v1.2.3