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

Windows
MacOS
Linux

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

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