From ae6293fe3758de664de6c1bec95048741d984418 Mon Sep 17 00:00:00 2001 From: Marius Peter Date: Fri, 7 Jun 2019 12:02:01 -0700 Subject: Reformat print_coord and save_coord data presentation --- creator.py | 33 ++++++++++++++++++++------------- main.py | 33 +++++++++++++++++++++++---------- 2 files changed, 43 insertions(+), 23 deletions(-) diff --git a/creator.py b/creator.py index 645ed9b..d5ff3ec 100644 --- a/creator.py +++ b/creator.py @@ -65,28 +65,35 @@ class Coordinates: def print_coord(self, round): """ - Print all the object's coordinates to the terminal. + Print all the component's coordinates to the terminal. This function's output is piped to the 'save_coord' function below. """ - print('Chord length', self.chord, sep='\n') - print('Semi-span') - print('x_u the upper x-coordinates') - print(np.around(self.x_u, round)) - print('y_u the upper y-coordinates') - print(np.around(self.y_u, round)) - print('x_l the lower x-coordinates') - print(np.around(self.x_l, round)) - print('y_l the lower y-coordinates') - print(np.around(self.y_l, round)) + print('============================') + print('Component:', type(self).__name__) + print('Chord length:', self.chord) + print('Semi-span:', self.semi_span) + print('============================') + print('x_u the upper x-coordinates:', + np.around(self.x_u, round), + sep='\n') + print('y_u the upper y-coordinates:', + np.around(self.y_u, round), + sep='\n') + print('x_l the lower x-coordinates:', + np.around(self.x_l, round), + sep='\n') + print('y_l the lower y-coordinates:', + np.around(self.y_l, round), + sep='\n') + print('\n') return None def save_coord(self, save_dir_path): """ Save all the object's coordinates (must be full path). """ - object_name = str(self.__name__) - file_name = 'airfoil_%s' % airfoil_number + file_name = str(type(self).__name__) full_path = os.path.join(save_dir_path, file_name + '.txt') file = open(full_path, 'w') sys.stdout = file diff --git a/main.py b/main.py index 4107054..a6e75a3 100644 --- a/main.py +++ b/main.py @@ -23,22 +23,35 @@ CHORD_LENGTH = 40 SEMI_SPAN = 200 POP_SIZE = 1 -SAVE_PATH = 'C:/Users/blend/Desktop/python/airfoils' +SAVE_PATH = 'C:/Users/blend/github/UCLA_MAE_154B/save' def main(): # Create coordinate system specific to airfoil dimensions. creator.Coordinates(CHORD_LENGTH, SEMI_SPAN) - for airfoil_number in range(1, POP_SIZE + 1): - foo = creator.Airfoil() - foo.naca(2412) - # foo.print_coord(4) - foo.spar = creator.Spar() - foo.spar.add_spar(foo.coordinates, 'aluminium', 0.15) - foo.spar.print_coord(4) - creator.plot(foo, foo.spar) - foo.save_values(SAVE_PATH) + # Interate through all wings in population. + for _ in range(1, POP_SIZE + 1): + # Create airfoil instance + af = creator.Airfoil() + # Define NACA airfoil coordinates + af.naca(2412) + # Print coordinates of af to terminal + af.print_coord(4) + # Create spar instance + af.spar = creator.Spar() + # Define the spar coordinates + af.spar.add_spar(af.coordinates, 'aluminium', 0.15) + # Print coordinates of af.spar to terminal + af.spar.print_coord(4) + # Plot components with matplotlib + creator.plot(af, af.spar) + + # Save component coordinates + af.save_coord(SAVE_PATH) + af.spar.save_coord(SAVE_PATH) + + # Print final execution time print("--- %s seconds ---" % (time.time() - start_time)) -- cgit v1.2.3