finalised branch :)

1 files changed, 10 insertions, 10 deletions

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)