doc

1 files changed, 12 insertions, 12 deletions

diff --git a/main.py b/main.py
index 5b7358d..1392218 100644
--- a/main.py
+++ b/main.py
@@ -66,8 +66,8 @@ def main():
         # Define NACA airfoil coordinates and mass
         af.add_naca(NACA_NUM)
         af.add_mass(AIRFOIL_MASS)
-        # af.info_print(2)
-        # af.info_save(SAVE_PATH, _)
+        af.info_print(2)
+        af.info_save(SAVE_PATH, _)
 
         # Create spar instance
         af.spar = creator.Spar()
@@ -78,8 +78,8 @@ 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_save(SAVE_PATH, _)
+        af.spar.info_print(2)
+        af.spar.info_save(SAVE_PATH, _)
 
         # Create stringer instance
         af.stringer = creator.Stringer()
@@ -92,24 +92,24 @@ 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_save(SAVE_PATH, _)
+        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(1, 1)
-        # eval.info_print(2)
-        # eval.info_save(SAVE_PATH, _)
-        # evaluator.plot_geom(eval)
-        # evaluator.plot_lift(eval)
+        eval.info_print(2)
+        eval.info_save(SAVE_PATH, _)
+        evaluator.plot_geom(eval)
+        evaluator.plot_lift(eval)
 
         pop = generator.Population(10)
 
-        # print(help(creator))
+        print(help(creator))
         # print(help(evaluator))
         # print(help(generator))