virtual public void UpdateFlightCondition()
{
ambientTherm = EngineThermodynamics.VesselAmbientConditions(vessel, useExtTemp);
}
private void FixedUpdate()
{
if (!HighLogic.LoadedSceneIsFlight || !vessel)
{
return;
}
if (vessel.altitude > vessel.mainBody.atmosphereDepth)
{
return;
}
int newCount = vessel.Parts.Count;
if (partsCount != newCount)
{
partsCount = newCount;
UpdatePartsList();
}
InletArea = 0d;
EngineArea = 0d;
OverallTPR = 0d;
AreaRatio = 0d;
for (int j = engineList.Count - 1; j >= 0; --j)
{
ModuleEnginesSolver e = engineList[j];
if ((object)e != null && e.EngineIgnited)
{
EngineArea += e.Need_Area;
}
}
for (int j = inletList.Count - 1; j >= 0; --j)
{
AJEInlet i = inletList[j];
if ((object)i != null)
{
double area = i.UsableArea();
InletArea += area;
OverallTPR += area * i.overallTPR;
}
}
if (InletArea > 0d)
{
if (EngineArea > 0d)
{
AreaRatio = Math.Min(1d, InletArea / EngineArea);
OverallTPR /= InletArea;
OverallTPR *= AreaRatio;
}
else
{
AreaRatio = 1d;
}
}
AmbientTherm = EngineThermodynamics.VesselAmbientConditions(vessel);
Mach = vessel.mach;
// Transform from static frame to vessel frame, increasing total pressure and temperature
if (vessel.srfSpeed < 0.01d)
{
InletTherm = AmbientTherm;
}
else
{
InletTherm = AmbientTherm.ChangeReferenceFrame(vessel.srfSpeed);
}
InletTherm.P *= OverallTPR; // TPR accounts for loss of total pressure by inlet
// Push parameters to each engine
for (int i = engineList.Count - 1; i >= 0; --i)
{
engineList[i].UpdateInletEffects(InletTherm, AreaRatio, OverallTPR);
}
}