change print_info and save_info to info_print and info_save ere

3 files changed, 18 insertions, 18 deletions

diff --git a/creator.py b/creator.py
index fd09e2c..a468c2d 100644
--- a/creator.py
+++ b/creator.py
@@ -69,7 +69,7 @@ class Coordinates:
     def __str__(self):
         return type(self).__name__
 
-    def print_info(self, round):
+    def info_print(self, round):
         '''
         Print all the component's coordinates to the terminal.
 
@@ -91,7 +91,7 @@ class Coordinates:
         print('z_l the lower z-coordinates:\n', np.around(self.z_l, round))
         return None
 
-    def save_info(self, save_dir_path, number):
+    def info_save(self, save_dir_path, number):
         '''
         Save all the object's coordinates (must be full path).
         '''
@@ -100,7 +100,7 @@ class Coordinates:
         full_path = os.path.join(save_dir_path, file_name)
         try:
             with open(full_path, 'w') as sys.stdout:
-                self.print_info(6)
+                self.info_print(6)
                 # This line required to reset behavior of sys.stdout
                 sys.stdout = sys.__stdout__
                 print('Successfully wrote to file {}'.format(full_path))
@@ -218,8 +218,8 @@ class Airfoil(Coordinates):
     def add_mass(self, mass):
         self.mass = mass
 
-    def print_info(self, round):
-        super().print_info(round)
+    def info_print(self, round):
+        super().info_print(round)
         print('x_c the camber x-coordinates:\n', np.around(self.x_u, round))
         print('z_c the camber z-coordinates:\n', np.around(self.x_u, round))
         return None
@@ -408,8 +408,8 @@ class Stringer(Coordinates):
         self.mass = len(self.x_u) * mass + len(self.x_l) * mass
         return None
 
-    def print_info(self, round):
-        super().print_info(round)
+    def info_print(self, round):
+        super().info_print(round)
         print('Stringer Area:\n', np.around(self.area, round))
         return None
 
diff --git a/evaluator.py b/evaluator.py
index c21ca2e..9a54120 100644
--- a/evaluator.py
+++ b/evaluator.py
@@ -53,7 +53,7 @@ class Airfoil:
         # Drag
         self.drag = []
 
-    def print_info(self, round):
+    def info_print(self, round):
         '''
         Print all the component's evaluated data to the terminal.
 
@@ -78,14 +78,14 @@ class Airfoil:
         print('Drag:\n', np.around(self.drag, round))
         return None
 
-    def save_info(self, save_dir_path, number):
+    def info_save(self, save_dir_path, number):
         '''Save all the object's coordinates (must be full path).'''
 
         file_name = 'airfoil_{}_eval.txt'.format(number)
         full_path = os.path.join(save_dir_path, file_name)
         try:
             with open(full_path, 'w') as sys.stdout:
-                self.print_info(6)
+                self.info_print(6)
                 # This line required to reset behavior of sys.stdout
                 sys.stdout = sys.__stdout__
                 print('Successfully wrote to file {}'.format(full_path))
diff --git a/main.py b/main.py
index 8805f11..a59fcff 100644
--- a/main.py
+++ b/main.py
@@ -58,8 +58,8 @@ def main():
         # Define NACA airfoil coordinates and mass
         af.add_naca(NACA_NUM)
         af.add_mass(AIRFOIL_MASS)
-        # af.print_info(2)
-        # af.save_info(SAVE_PATH, _)
+        # af.info_print(2)
+        # af.info_save(SAVE_PATH, _)
 
         # Create spar instance
         af.spar = creator.Spar()
@@ -67,8 +67,8 @@ 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.save_info(SAVE_PATH, _)
+        # af.spar.info_print(2)
+        # af.spar.info_save(SAVE_PATH, _)
 
         # Create stringer instance
         af.stringer = creator.Stringer()
@@ -76,8 +76,8 @@ 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.save_info(SAVE_PATH, _)
+        # af.stringer.info_print(2)
+        # af.stringer.info_save(SAVE_PATH, _)
 
         # Plot components with matplotlib
         # af.plot()
@@ -86,8 +86,8 @@ def main():
         eval = evaluator.Airfoil(af)
         # The analysis is performed in the evaluator.py module.
         eval.analysis()
-        eval.print_info(2)
-        # eval.save_info(SAVE_PATH, _)
+        eval.info_print(2)
+        # eval.info_save(SAVE_PATH, _)
         # eval.plot()
 
     # Print final execution time