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| author | blendoit <blendoit@gmail.com> | 2019-09-28 15:59:06 -0700 |
|---|---|---|
| committer | blendoit <blendoit@gmail.com> | 2019-09-28 15:59:06 -0700 |
| commit | 68aa008345d4041402020d8343b72fa155839e6f (patch) | |
| tree | 2016cfb8eec0f9558854c76cafbe4bb7c2e24972 /tools/creator.py | |
| parent | 91bc68f91306b07a2801f87532c56e9c4504f9a4 (diff) | |
Change README.md to org
Better README capacity in org-mode
Diffstat (limited to 'tools/creator.py')
| -rw-r--r-- | tools/creator.py | 18 |
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[_] |