FAerofoil::CalcLiftCoefficient

Returns lift coefficient for the current angle of attack of the aerofoil surface Cheating by making control surface part of entire aerofoil movement

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References

Module	ChaosVehiclesCore
Header	/Engine/Source/Runtime/Experimental/ChaosVehicles/ChaosVehiclesCore/Public/AerofoilSystem.h
Include	#include "AerofoilSystem.h"
Source	/Engine/Source/Runtime/Experimental/ChaosVehicles/ChaosVehiclesCore/Private/AerofoilSystem.cpp

Syntax

float CalcLiftCoefficient
(
float InAngleOfAttack,
float InControlSurfaceAngle
)

Remarks

Returns lift coefficient for the current angle of attack of the aerofoil surface Cheating by making control surface part of entire aerofoil movement