diff options
| -rw-r--r-- | creator.py | 9 | ||||
| -rw-r--r-- | main.py | 5 |
2 files changed, 7 insertions, 7 deletions
@@ -242,7 +242,7 @@ class Spar(Coordinates): def __init__(self):
super().__init__(parent.chord, parent.semi_span)
- def add_spar(self, coordinates, material, spar_x):
+ def add_spar(self, coordinates, spar_x):
"""
Add a single spar at the % chord location given to function.
@@ -271,7 +271,6 @@ class Spar(Coordinates): self.y_u.append(y_u[spar_x_u])
self.x_l.append(x_l[spar_x_l])
self.y_l.append(y_l[spar_x_l])
- self.spar_material = material
return None
@@ -286,7 +285,7 @@ class Stringer(): self.stringer_y_l = []
self.stringer_mat = []
- def add_stringers(self, material, *density):
+ def add_stringers(self, *density):
"""
Add stringers to the wing from their distribution density between spars.
First half of density[] concerns stringer distribution on
@@ -347,8 +346,8 @@ def plot(airfoil, spar): # Plot spars
try:
for _ in range(0, len(spar.x_u)):
- x = (spar.spar_x_u[_], spar.spar_x_l[_])
- y = (spar.spar_y_u[_], spar.spar_y_l[_])
+ x = (spar.x_u[_], spar.x_l[_])
+ y = (spar.y_u[_], spar.y_l[_])
plt.plot(x, y, '.-', color='b', label='spar')
plt.legend()
except:
@@ -19,7 +19,7 @@ import random import time start_time = time.time() -CHORD_LENGTH = 40 +CHORD_LENGTH = 100 SEMI_SPAN = 200 POP_SIZE = 1 @@ -41,7 +41,8 @@ def main(): # Create spar instance af.spar = creator.Spar() # Define the spar coordinates - af.spar.add_spar(af.coordinates, 'aluminium', 0.15) + af.spar.add_spar(af.coordinates, 0.15) + af.spar.add_spar(af.coordinates, 0.55) # Print coordinates of af.spar to terminal af.spar.print_coord(4) # Plot components with matplotlib |