summaryrefslogtreecommitdiff
path: root/tools
diff options
context:
space:
mode:
Diffstat (limited to 'tools')
-rw-r--r--tools/creator.py18
1 files changed, 9 insertions, 9 deletions
diff --git a/tools/creator.py b/tools/creator.py
index 01f73ad..6d074f8 100644
--- a/tools/creator.py
+++ b/tools/creator.py
@@ -37,7 +37,7 @@ import matplotlib.pyplot as plt
class Airfoil:
"""This class represents a single NACA airfoil.
- Please note: the coordinates are saved as two lists
+ The coordinates are saved as two lists
for the x- and z-coordinates. The coordinates start at
the leading edge, travel over the airfoil's upper edge,
then loop back to the leading edge via the lower edge.
@@ -69,7 +69,7 @@ class Airfoil:
else:
cls.chord = 20
print('Chord too small, using minimum value of 20.')
- cls.semi_span = semi_span
+ cls.semi_span = semi_span
return Airfoil()
def __str__(self):
@@ -175,7 +175,7 @@ class Airfoil:
for k, v in self.__dict__.items():
if type(v) != list:
print('{}:\n'.format(k), v)
- print(num_of_dashes * '-')
+ print(num_of_dashes * '-')
for k, v in self.__dict__.items():
if type(v) == list:
print('{}:\n'.format(k), np.around(v, round))
@@ -251,7 +251,7 @@ class Spar(Airfoil):
self.x_end.append(self.x[_][1])
self.z_start.append(self.z[_][0])
self.z_end.append(self.z[_][1])
- self.thickness = thickness
+ self.thickness = thickness
return None
@@ -296,8 +296,8 @@ class Stringer(Airfoil):
self.x.append(airfoil.x[i])
self.z.append(airfoil.z[i])
x += interval
- # Add upper stringers from first spar until last spar
- # TODO: stringer placement if only one spar is created
+ # Add upper stringers from first spar until last spar
+ # TODO: stringer placement if only one spar is created
interval = (airfoil.spar.x[-1][0]
- airfoil.spar.x[0][0]) / (stringer_u_2 + 1)
x = interval + airfoil.spar.x[0][0]
@@ -316,7 +316,7 @@ class Stringer(Airfoil):
self.x.append(airfoil.x[-i])
self.z.append(airfoil.z[-i])
x += interval
- # Add lower stringers from first spar until last spar
+ # Add lower stringers from first spar until last spar
interval = (airfoil.spar.x[-1][1]
- airfoil.spar.x[0][1]) / (stringer_l_2 + 1)
x = interval + airfoil.spar.x[0][1]
@@ -342,7 +342,7 @@ class Stringer(Airfoil):
self.x_end.append(self.x[_ + 1])
self.z_start.append(self.z[_])
self.z_end.append(self.z[_ + 1])
- self.thickness = thickness
+ self.thickness = thickness
return None
def info_print(self, round):
@@ -379,7 +379,7 @@ def plot_geom(airfoil, view: False):
ax.plot(x, y, '-', color='y', linewidth='4')
except AttributeError:
print('No spars to plot.')
- # Plot stringers
+ # Plot stringers
try:
for _ in range(0, len(airfoil.stringer.x)):
x = airfoil.stringer.x[_]
Copyright 2019--2024 Marius PETER