private void CalculateAndApplyVesselAeroProperties()
{
float atmDensity = (float)vessel.atmDensity;
if (atmDensity <= 0)
{
MachNumber = 0;
ReynoldsNumber = 0;
return;
}
MachNumber = vessel.mach;
ReynoldsNumber = FARAeroUtil.CalculateReynoldsNumber(vessel.atmDensity,
Length,
vessel.srfSpeed,
MachNumber,
FlightGlobals.getExternalTemperature((float)vessel
.altitude,
vessel.mainBody),
vessel.mainBody.atmosphereAdiabaticIndex);
float skinFrictionDragCoefficient = (float)FARAeroUtil.SkinFrictionDrag(ReynoldsNumber, MachNumber);
float pseudoKnudsenNumber = (float)(MachNumber / (ReynoldsNumber + MachNumber));
Vector3 frameVel = Krakensbane.GetFrameVelocityV3f();
//start from the top and come down to improve performance if it needs to remove anything
for (int i = _currentAeroModules.Count - 1; i >= 0; i--)
{
FARAeroPartModule m = _currentAeroModules[i];
if (m != null && m.part != null && m.part.partTransform != null)
{
m.UpdateVelocityAndAngVelocity(frameVel);
}
else
{
_currentAeroModules.RemoveAt(i);
}
}
foreach (FARAeroSection aeroSection in _currentAeroSections)
{
aeroSection.FlightCalculateAeroForces((float)MachNumber,
(float)(ReynoldsNumber / Length),
pseudoKnudsenNumber,
skinFrictionDragCoefficient);
}
_vesselIntakeRamDrag.ApplyIntakeRamDrag((float)MachNumber, vessel.srf_velocity.normalized);
foreach (FARAeroPartModule m in _currentAeroModules)
{
m.ApplyForces();
}
}
private void CalculateAndApplyVesselAeroProperties()
{
float atmDensity = (float)_vessel.atmDensity;
if (atmDensity <= 0)
{
machNumber = 0;
reynoldsNumber = 0;
return;
}
machNumber = _vessel.mach;
reynoldsNumber = FARAeroUtil.CalculateReynoldsNumber(_vessel.atmDensity, Length, _vessel.srfSpeed, machNumber, FlightGlobals.getExternalTemperature((float)_vessel.altitude, _vessel.mainBody), _vessel.mainBody.atmosphereAdiabaticIndex);
float skinFrictionDragCoefficient = (float)FARAeroUtil.SkinFrictionDrag(reynoldsNumber, machNumber);
Vector3 frameVel = Krakensbane.GetFrameVelocityV3f();
if (_updateQueued) //only happens if we have an voxelization scheduled, then we need to check for null
{
for (int i = _currentAeroModules.Count - 1; i >= 0; i--) //start from the top and come down to improve performance if it needs to remove anything
{
FARAeroPartModule m = _currentAeroModules[i];
if (m != null)
{
m.UpdateVelocityAndAngVelocity(frameVel);
}
else
{
_currentAeroModules.RemoveAt(i);
i++;
}
}
}
else //otherwise, we don't need to do Unity's expensive "is this part dead" null-check
{
for (int i = _currentAeroModules.Count - 1; i >= 0; i--) //start from the top and come down to improve performance if it needs to remove anything
{
FARAeroPartModule m = _currentAeroModules[i];
m.UpdateVelocityAndAngVelocity(frameVel);
}
}
for (int i = 0; i < _currentAeroSections.Count; i++)
{
_currentAeroSections[i].FlightCalculateAeroForces(atmDensity, (float)machNumber, (float)(reynoldsNumber / Length), skinFrictionDragCoefficient);
}
_vesselIntakeRamDrag.ApplyIntakeRamDrag((float)machNumber, _vessel.srf_velocity.normalized, (float)_vessel.dynamicPressurekPa);
for (int i = 0; i < _currentAeroModules.Count; i++)
{
FARAeroPartModule m = _currentAeroModules[i];
m.ApplyForces();
}
}
private void CalculateAndApplyVesselAeroProperties()
{
float atmDensity = (float)_vessel.atmDensity;
if (atmDensity <= 0)
{
machNumber = 0;
reynoldsNumber = 0;
return;
}
machNumber = _vessel.mach;
reynoldsNumber = FARAeroUtil.CalculateReynoldsNumber(_vessel.atmDensity, Length, _vessel.srfSpeed, machNumber, FlightGlobals.getExternalTemperature((float)_vessel.altitude, _vessel.mainBody), _vessel.mainBody.atmosphereAdiabaticIndex);
float skinFrictionDragCoefficient = (float)FARAeroUtil.SkinFrictionDrag(reynoldsNumber, machNumber);
Vector3 frameVel = Krakensbane.GetFrameVelocityV3f();
for (int i = 0; i < _currentAeroModules.Count; i++)
{
FARAeroPartModule m = _currentAeroModules[i];
if (m != null)
{
m.UpdateVelocityAndAngVelocity(frameVel);
}
else
{
_currentAeroModules.RemoveAt(i);
i--;
}
}
for (int i = 0; i < _currentAeroSections.Count; i++)
{
_currentAeroSections[i].FlightCalculateAeroForces(atmDensity, (float)machNumber, (float)(reynoldsNumber / Length), skinFrictionDragCoefficient);
}
_vesselIntakeRamDrag.ApplyIntakeRamDrag((float)machNumber, _vessel.srf_velocity.normalized, (float)_vessel.dynamicPressurekPa);
for (int i = 0; i < _currentAeroModules.Count; i++)
{
FARAeroPartModule m = _currentAeroModules[i];
if ((object)m != null)
{
m.ApplyForces();
}
}
}
