public void DoEngineFit()
{
SolverJet jetEngine = engineSolver as SolverJet;
jetEngine.FitEngine(dryThrust * 1000d, drySFC, wetThrust * 1000d, idleNPR, defaultTPR: defaultTPR);
Area = (float)jetEngine.GetAref();
FHV = (float)jetEngine.GetFHV();
TAB = (float)jetEngine.GetTAB();
minThrottle = (float)jetEngine.GetMinThrottle();
turbineAreaRatio = (float)jetEngine.GetTurbineAreaRatio();
PushAreaToInlet();
}
public override void CreateEngine()
{
// bool DREactive = AssemblyLoader.loadedAssemblies.Any(
// a => a.assembly.GetName().Name.Equals("DeadlyReentry.dll", StringComparison.InvariantCultureIgnoreCase));
// heatProduction = (float)part.maxTemp * 0.1f;
engineSolver = solverJet = new SolverJet();
solverJet.InitializeOverallEngineData(
Area,
BPR,
CPR,
FPR,
Mdes,
Tdes,
eta_c,
eta_t,
eta_n,
FHV,
TIT,
TAB,
minThrottle,
turbineAreaRatio,
exhaustMixer,
adjustableNozzle,
unifiedThrottle
);
useAtmCurve = atmChangeFlow = useVelCurve = useAtmCurveIsp = useVelCurveIsp = false;
maxEngineTemp = maxT3;
if (autoignitionTemp < 0f || float.IsInfinity(autoignitionTemp))
{
autoignitionTemp = 500f; // Autoignition of Kerosene is 493.15K
}
PushAreaToInlet();
// set heat production
heatProduction = Mathf.Min(10f, (1f - eta_c) * (1f - eta_t) * (1f - eta_n) * (10000f + TAB * 10f) / (1f + BPR * 0.5f));
}
