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FAerofoil::GetForce

Returns the combined force of lift and drag at an aerofoil in world coordinates for direct application to the aircrafts rigid body.

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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

FVector GetForce
(
    FTransform & BodyTransform,
    const FVector & v,
    float Altitude,
    float DeltaTime
)

Remarks

Returns the combined force of lift and drag at an aerofoil in world coordinates for direct application to the aircrafts rigid body.

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