private static void Reset(SimulatedVessel obj)
{
SimulatedPart.Release(obj.parts);
obj.parts.Clear();
SimulatedLiftingSurface.Release(obj.surfaces);
obj.surfaces.Clear();
SimulatedControlSurface.Release(obj.ctrls);
obj.ctrls.Clear();
SimulatedEngine.Release(obj.engines);
obj.engines.Clear();
}
protected static void Reset(PartCollection obj)
{
SimulatedPart.Release(obj.parts);
obj.parts.Clear();
SimulatedLiftingSurface.Release(obj.surfaces);
obj.surfaces.Clear();
SimulatedControlSurface.Release(obj.ctrls);
obj.ctrls.Clear();
SimulatedEngine.Release(obj.engines);
obj.engines.Clear();
PartCollection.Release(obj.partCollections);
obj.partCollections.Clear();
}
private void GenerateHighlightingData(ShipConstruct ship, CelestialBody body, float altitude, float speed, float aoa)
{
float mach, atmDensity;
lock (body)
{
atmDensity = (float)Extensions.KSPClassExtensions.GetDensity(body, altitude);
mach = speed / (float)body.GetSpeedOfSound(body.GetPressure(altitude), atmDensity);
}
int count = ship.parts.Count;
highlightingData = new PartAeroData[count];
Vector3 inflow = AeroPredictor.InflowVect(aoa);
float pseudoReDragMult;
lock (PhysicsGlobals.DragCurvePseudoReynolds)
pseudoReDragMult = PhysicsGlobals.DragCurvePseudoReynolds.Evaluate(atmDensity * speed);
for (int i = 0; i < count; i++)
{
if (WindTunnelSettings.HighlightIgnoresLiftingSurfaces && ship.parts[i].HasModuleImplementing <ModuleLiftingSurface>())
{
highlightingData[i] = new PartAeroData(0, 0, ship.parts[i].mass);
continue;
}
VesselCache.SimulatedPart simPart = VesselCache.SimulatedPart.Borrow(ship.parts[i], null);
Vector3 partForce = simPart.GetAero(inflow, mach, pseudoReDragMult);
ModuleLiftingSurface liftingSurface = ship.parts[i].FindModuleImplementing <ModuleLiftingSurface>();
if (liftingSurface != null)
{
VesselCache.SimulatedLiftingSurface simLiftSurf = VesselCache.SimulatedLiftingSurface.Borrow(liftingSurface, simPart);
partForce += simLiftSurf.GetForce(inflow, mach);
simLiftSurf.Release();
}
simPart.Release();
//Vector3 partForce = highlightingVessel.parts[i].GetAero(inflow, mach, pseudoReDragMult);
//Vector3 partForce = StockAeroUtil.SimAeroForce(body, new ShipConstruct("test", "", new List<Part>() { EditorLogic.fetch.ship.parts[i] }), inflow * speed, altitude);
partForce = AeroPredictor.ToFlightFrame(partForce, aoa); // (Quaternion.AngleAxis((aoa * 180 / Mathf.PI), Vector3.left) * partForce);
highlightingData[i] = new PartAeroData(Math.Abs(partForce.z), Math.Abs(partForce.y), ship.parts[i].mass);
}
}