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examples/rectangular_wing.jl
@@ -3,9 +3,9 @@ using ControlPlots
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using VortexStepMethod
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# Step 1: Define wing parameters
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-n_panels = 20 # Number of panels
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-span = 20.0 # Wing span [m]
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-chord = 1.0 # Chord length [m]
+n_panels = 20 # Number of panels
+span = 20.0 # Wing span [m]
+chord = 1.0 # Chord length [m]
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Umag = 20.0 # Magnitude of inflow velocity [m/s]
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density = 1.225 # Air density [kg/m³]
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alpha_deg = 30.0 # Angle of attack [degrees]
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