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();
 }
 public void ClearAeroSection()
 {
     xForcePressureAoA0 = null;
     xForcePressureAoA180 = null;
     xForceSkinFriction = null;
     partData = null;
 }