remove unused exception catching

2 files changed, 24 insertions, 29 deletions

diff --git a/creator.py b/creator.py
index 3f6cbd8..6cc2268 100644
--- a/creator.py
+++ b/creator.py
@@ -243,7 +243,7 @@ class Spar(Coordinates):
         # Scaled spar location with regards to chord
         loc = spar_x * self.chord
         # bisect_left: returns index of first value in x_u > loc.
-        # This ensures that the spar coordinates intersect with airfoil surface.
+        # Ensures that the spar coordinates intersect with airfoil surface.
         spar_x_u = bi.bisect_left(x_u, loc)  # index of spar's x_u
         spar_x_l = bi.bisect_left(x_l, loc)  # index of spar's x_l
         # These x and y coordinates are assigned to the spar, NOT airfoil.
@@ -374,29 +374,22 @@ def plot(airfoil, spar, stringer):
     plt.plot(airfoil.x_l, airfoil.z_l, '', color='b', linewidth='1')
 
     # Plot spars
-    try:
-        for _ in range(0, len(spar.x_u)):
-            x = (spar.x_u[_], spar.x_l[_])
-            y = (spar.z_u[_], spar.z_l[_])
-            plt.plot(x, y, '.-', color='b')
-            # plt.legend()
-    except:
-        print('Did not plot spars. Were they added?')
+    for _ in range(0, len(spar.x_u)):
+        x = (spar.x_u[_], spar.x_l[_])
+        y = (spar.z_u[_], spar.z_l[_])
+        plt.plot(x, y, '.-', color='b')
 
     # Plot stringers
-    try:
-        # Upper stringers
-        for _ in range(0, len(stringer.x_u)):
-            x = stringer.x_u[_]
-            y = stringer.z_u[_]
-            plt.plot(x, y, '.', color='y')
-        # Lower stringers
-        for _ in range(0, len(stringer.x_l)):
-            x = stringer.x_l[_]
-            y = stringer.z_l[_]
-            plt.plot(x, y, '.', color='y')
-    except:
-        print('Unable to plot stringers. Were they created?')
+    # Upper stringers
+    for _ in range(0, len(stringer.x_u)):
+        x = stringer.x_u[_]
+        y = stringer.z_u[_]
+        plt.plot(x, y, '.', color='y')
+    # Lower stringers
+    for _ in range(0, len(stringer.x_l)):
+        x = stringer.x_l[_]
+        y = stringer.z_l[_]
+        plt.plot(x, y, '.', color='y')
 
     # Graph formatting
     plt.gca().set_aspect('equal', adjustable='box')
diff --git a/main.py b/main.py
index 9d9db82..fe5bb10 100644
--- a/main.py
+++ b/main.py
@@ -21,10 +21,12 @@ import random
 import time
 start_time = time.time()
 
-CHORD_LENGTH = 10
+# Airfoil dimensions
+NACA_NUM = 4412
+CHORD_LENGTH = 100
 SEMI_SPAN = 200
 
-# m=Mass
+# Component masses
 AIRFOIL_MASS = 100  # lbs
 SPAR_MASS = 10  # lbs
 STRINGER_MASS = 5  # lbs
@@ -54,9 +56,9 @@ def main():
         # Create airfoil instance
         af = creator.Airfoil()
         # Define NACA airfoil coordinates and mass
-        af.add_naca(2412)
+        af.add_naca(NACA_NUM)
         af.add_mass(AIRFOIL_MASS)
-        af.print_info(2)
+        # af.print_info(2)
 
         # Create spar instance
         af.spar = creator.Spar()
@@ -64,7 +66,7 @@ def main():
         af.spar.add_coord(af.coord, 0.15)
         af.spar.add_coord(af.coord, 0.55)
         af.spar.add_mass(SPAR_MASS)
-        af.spar.print_info(2)
+        # af.spar.print_info(2)
 
         # Create stringer instance
         af.stringer = creator.Stringer()
@@ -72,10 +74,10 @@ def main():
         af.stringer.add_coord(af.coord, af.spar.coord, 4, 7, 5, 6)
         af.stringer.add_area(STRINGER_AREA)
         af.stringer.add_mass(STRINGER_MASS)
-        af.stringer.print_info(2)
+        # af.stringer.print_info(2)
 
         # Plot components with matplotlib
-        # creator.plot(af, af.spar, af.stringer)
+        creator.plot(af, af.spar, af.stringer)
 
         # Save component info
         af.save_info(SAVE_PATH, _)