FAerofoil::CalcDragCoefficient

Returns drag coefficient for the current angle of attack of the aerofoil surface

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 CalcDragCoefficient
(
    float InAngleOfAttack,
    float InControlSurfaceAngle
)

Remarks

Returns drag coefficient for the current angle of attack of the aerofoil surface

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