Navigation
API > API/Runtime > API/Runtime/ChaosVehiclesCore > API/Runtime/ChaosVehiclesCore/FAerofoil
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 |
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.