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 |
float CalcDynamicPressure
&40;
float VelocitySqr,
float InAltitude
&41;
Remarks
Dynamic air pressure = 0.5 * AirDensity * Vsqr This function reduces the dynamic pressure in a linear fashion with altitude between MinCeiling & MaxCeiling in order to limit the aircrafts altitude with a 'natural feel' without having a hard limit