14 #define MaxCLDelta 0.800f 15 #define MaxCDDelta 0.060f 22 #define maxDragIncreaseApproachingMachC 3.7177f // 4.7177 minus 1 which is the default 88 void Update(
float fElapsedTime);
float EngineThrustOutput[MAX_ENGINES]
float rollAccelerationSnapshot
float airframeTempCelsius
void Update(float fElapsedTime)
float yawAccelerationSnapshot
static float CalculateLiftCoefficient(AirfoilType type, float aoaRad, float CLDelta)
float pitchAccelerationSnapshot
static void GetFrictionCoefficients(unsigned char type, float *rollingResistance, float *roughness)
D3DXVECTOR3 relativeWindTrueKms
float ThrustReverserOutput[MAX_ENGINES]
const D3DXVECTOR3 centerC
static float CalculateDragCoefficient(AirfoilType type, float aoa, float CDDelta)
D3DXVECTOR3 windVectorTrueKms
float GetTotalThrust() const
D3DXVECTOR3 oldOdoPosition
propulsion(Viewscreen *ptr)