public void ClearAeroSection() { xForcePressureAoA0 = null; xForcePressureAoA180 = null; xForceSkinFriction = null; partData = null; }
public FARAeroSection() { xForcePressureAoA0 = new FARFloatCurve(6); xForcePressureAoA180 = new FARFloatCurve(6); xForceSkinFriction = new FARFloatCurve(3); partData = new List <PartData>(); handledAeroModulesIndexDict = new Dictionary <FARAeroPartModule, int>(); GenerateCrossFlowDragCurve(); }
public FARAeroSection() { xForcePressureAoA0 = new FARFloatCurve(6); xForcePressureAoA180 = new FARFloatCurve(6); xForceSkinFriction = new FARFloatCurve(3); partData = new List<PartData>(); if (crossFlowDragMachCurve == null) GenerateCrossFlowDragCurve(); }
public FARAeroSection() { xForcePressureAoA0 = new FARFloatCurve(6); xForcePressureAoA180 = new FARFloatCurve(6); xForceSkinFriction = new FARFloatCurve(3); partData = new List <PartData>(); if (crossFlowDragMachCurve == null) { GenerateCrossFlowDragCurve(); } }
public FARAeroSection() { xForcePressureAoA0 = new FARFloatCurve(6); xForcePressureAoA180 = new FARFloatCurve(6); xForceSkinFriction = new FARFloatCurve(3); partData = new List<PartData>(); handledAeroModulesIndexDict = new Dictionary<FARAeroPartModule, int>(); if (crossFlowDragMachCurve == null) GenerateCrossFlowDragCurve(); }