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1 parent d4a661e commit 2e6dc28Copy full SHA for 2e6dc28
rocketpy/AeroSurfaces.py
@@ -633,22 +633,22 @@ def rollInfo(self):
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self.rollForcingInterferenceFactor
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)
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- #lacks a title for the plot
+ # lacks a title for the plot
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self.rollParameters[0]()
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self.rollParameters[1]()
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return None
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def airfoilPlots(self):
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-
+
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if self.airfoil is not None:
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airfoilCl = Function(
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self.airfoil[0],
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- inputs = "angle of attack",
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- outputs = "lift coefficient",
+ inputs="angle of attack",
+ outputs="lift coefficient",
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interpolation="linear",
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- extrapolation = None,
+ extrapolation=None,
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airfoilCl.plot1D()
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