From 6946f206a17c5155fc4e517d72c5674fb8cd759b Mon Sep 17 00:00:00 2001
From: Marius Peter <blendoit@gmail.com>
Date: Fri, 21 Jun 2019 19:40:57 -0700
Subject: better print_info() file titles

---
 creator.py   |  9 ++++++---
 evaluator.py |  9 ++++++---
 main.py      | 12 +++++-------
 3 files changed, 17 insertions(+), 13 deletions(-)

diff --git a/creator.py b/creator.py
index 1a4ddb7..fd09e2c 100644
--- a/creator.py
+++ b/creator.py
@@ -75,13 +75,16 @@ class Coordinates:
 
         This function's output is piped to the 'save_coord' function below.
         '''
-        print(20 * '-')
-        print('    CREATOR DATA    ')
+        name = '    CREATOR DATA    '
+        num_of_dashes = len(name)
+
+        print(num_of_dashes * '-')
+        print(name)
         print('Component:', str(self))
         print('Chord length:', self.chord)
         print('Semi-span:', self.semi_span)
         print('Mass:', self.mass)
-        print(20 * '-')
+        print(num_of_dashes * '-')
         print('x_u the upper x-coordinates:\n', np.around(self.x_u, round))
         print('z_u the upper z-coordinates:\n', np.around(self.z_u, round))
         print('x_l the lower x-coordinates:\n', np.around(self.x_l, round))
diff --git a/evaluator.py b/evaluator.py
index 01647a6..c21ca2e 100644
--- a/evaluator.py
+++ b/evaluator.py
@@ -60,14 +60,17 @@ class Airfoil:
         This function's output is piped to the 'save_data' function below.
         '''
 
-        print(22 * '-')
-        print('    EVALUATOR DATA    ')
+        name = '    CREATOR DATA    '
+        num_of_dashes = len(name)
+
+        print(num_of_dashes * '-')
+        print(name)
         print('Evaluating:', self.airfoil)
         print('Chord length:', self.chord)
         print('Semi-span:', self.semi_span)
         print('Total airfoil mass:', self.mass_total)
         print('Centroid location:', np.around(self.centroid, round + 1))
-        print(22 * '-')
+        print(num_of_dashes * '-')
         print('Rectangular lift:\n', np.around(self.lift_rectangular, round))
         print('Elliptical lift:\n', np.around(self.lift_elliptical, round))
         print('Combined lift:\n', np.around(self.lift, round))
diff --git a/main.py b/main.py
index 2cf4a2e..8805f11 100644
--- a/main.py
+++ b/main.py
@@ -59,6 +59,7 @@ def main():
         af.add_naca(NACA_NUM)
         af.add_mass(AIRFOIL_MASS)
         # af.print_info(2)
+        # af.save_info(SAVE_PATH, _)
 
         # Create spar instance
         af.spar = creator.Spar()
@@ -67,6 +68,7 @@ def main():
         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, _)
 
         # Create stringer instance
         af.stringer = creator.Stringer()
@@ -75,22 +77,18 @@ def main():
         af.stringer.add_area(STRINGER_AREA)
         af.stringer.add_mass(STRINGER_MASS)
         # af.stringer.print_info(2)
+        # af.stringer.save_info(SAVE_PATH, _)
 
         # Plot components with matplotlib
         # af.plot()
 
-        # Save component info
-        # af.save_info(SAVE_PATH, _)
-        # af.spar.save_info(SAVE_PATH, _)
-        # af.stringer.save_info(SAVE_PATH, _)
-
         # evaluator.Evaluator instance contains airfoil analysis results.
         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.plot()
+        # eval.save_info(SAVE_PATH, _)
+        # eval.plot()
 
     # Print final execution time
     print("--- %s seconds ---" % (time.time() - start_time))
-- 
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