AddPly(NXOpen.PhysicalMaterial material, double thickness, NXOpen.Unit thicknessUnit, double angle, NXOpen.Unit angleUnit) | NXOpen.CAE.AeroStructures.LocalLaminate | inline |
AddPlyByMaterialName(string materialName, double thickness, NXOpen.Unit thicknessUnit, double angle, NXOpen.Unit angleUnit) | NXOpen.CAE.AeroStructures.LocalLaminate | inline |
AsyncProcessMessage(IMessage msg, IMessageSink replySink) | NXOpen.Utilities.NXRemotableObject | inline |
CreateLocalLaminateByCopy() | NXOpen.CAE.AeroStructures.Laminate | inline |
Dispose() | NXOpen.TransientObject | inline |
FreeResource() | NXOpen.CAE.AeroStructures.LocalLaminate | inlineprotectedvirtual |
GetABD() | NXOpen.CAE.AeroStructures.Laminate | inline |
GetBendingShearModulus() | NXOpen.CAE.AeroStructures.Laminate | inline |
GetBendingYoungsModulus() | NXOpen.CAE.AeroStructures.Laminate | inline |
GetBottomFiberDistance() | NXOpen.CAE.AeroStructures.Laminate | inline |
GetInterlaminarShearStress(bool usePlyCoordinates, double[] opTemp, double[] nxx, double[] nyy, double[] nxy, double[] mxx, double[] myy, double[] mxy, double[] tsx, double[] tsy, out NXOpen.GeneralScalarTable stressYz, out NXOpen.GeneralScalarTable stressZx) | NXOpen.CAE.AeroStructures.Laminate | inline |
GetLaminateAngle() | NXOpen.CAE.AeroStructures.Laminate | inline |
GetMaterialNames(out string[] materialNames) | NXOpen.CAE.AeroStructures.Laminate | inline |
GetMaterialPlyCount(int materialIndex, out int[] plies) | NXOpen.CAE.AeroStructures.Laminate | inline |
GetMaterialThickness(int materialIndex, out double[] thicknesses) | NXOpen.CAE.AeroStructures.Laminate | inline |
GetMid1() | NXOpen.CAE.AeroStructures.Laminate | inline |
GetMid2() | NXOpen.CAE.AeroStructures.Laminate | inline |
GetMid3() | NXOpen.CAE.AeroStructures.Laminate | inline |
GetMid4() | NXOpen.CAE.AeroStructures.Laminate | inline |
GetOrientations(out double[] orientations) | NXOpen.CAE.AeroStructures.Laminate | inline |
GetPlyAngle(int plyIndex) | NXOpen.CAE.AeroStructures.Laminate | inline |
GetPlyAngles(out double[] values) | NXOpen.CAE.AeroStructures.Laminate | inline |
GetPlyId(int plyIndex) | NXOpen.CAE.AeroStructures.Laminate | inline |
GetPlyIds(out int[] ids) | NXOpen.CAE.AeroStructures.Laminate | inline |
GetPlyMaterial(int plyIndex) | NXOpen.CAE.AeroStructures.Laminate | inline |
GetPlyMaterialName(int plyIndex) | NXOpen.CAE.AeroStructures.Laminate | inline |
GetPlyMaterialNames(out string[] names) | NXOpen.CAE.AeroStructures.Laminate | inline |
GetPlyMaterials(out NXOpen.PhysicalMaterial[] materials) | NXOpen.CAE.AeroStructures.Laminate | inline |
GetPlyThickness(int plyIndex) | NXOpen.CAE.AeroStructures.Laminate | inline |
GetPlyThicknesses(out double[] values) | NXOpen.CAE.AeroStructures.Laminate | inline |
GetPoissonsRatio() | NXOpen.CAE.AeroStructures.Laminate | inline |
GetReferencePlane() | NXOpen.CAE.AeroStructures.Laminate | inline |
GetReferenceTemperature() | NXOpen.CAE.AeroStructures.Laminate | inline |
GetShearModulus() | NXOpen.CAE.AeroStructures.Laminate | inline |
GetSpecificHeat() | NXOpen.CAE.AeroStructures.Laminate | inline |
GetStiffnessA() | NXOpen.CAE.AeroStructures.Laminate | inline |
GetStiffnessB() | NXOpen.CAE.AeroStructures.Laminate | inline |
GetStiffnessD() | NXOpen.CAE.AeroStructures.Laminate | inline |
GetStrainPerPly(bool usePlyCoordinates, double[] opTemp, double[] nxx, double[] nyy, double[] nxy, double[] mxx, double[] myy, double[] mxy, out NXOpen.GeneralScalarTable xxStrain, out NXOpen.GeneralScalarTable yyStrain, out NXOpen.GeneralScalarTable xyStrain) | NXOpen.CAE.AeroStructures.Laminate | inline |
GetStressPerPly(bool usePlyCoordinates, double[] opTemp, double[] nxx, double[] nyy, double[] nxy, double[] mxx, double[] myy, double[] mxy, out NXOpen.GeneralScalarTable xxStress, out NXOpen.GeneralScalarTable yyStress, out NXOpen.GeneralScalarTable xyStress) | NXOpen.CAE.AeroStructures.Laminate | inline |
GetThermalConductivityCoeff() | NXOpen.CAE.AeroStructures.Laminate | inline |
GetThermalExpansionCoeff() | NXOpen.CAE.AeroStructures.Laminate | inline |
GetTransverseShear() | NXOpen.CAE.AeroStructures.Laminate | inline |
GetYoungsModulus() | NXOpen.CAE.AeroStructures.Laminate | inline |
Handle | NXOpen.TransientObject | |
IsBalanced | NXOpen.CAE.AeroStructures.Laminate | |
IsInverted() | NXOpen.CAE.AeroStructures.Laminate | inline |
IsReversed() | NXOpen.CAE.AeroStructures.Laminate | inline |
IsSymmetric | NXOpen.CAE.AeroStructures.Laminate | |
IsUsingPlyMaterial(int plyIndex) | NXOpen.CAE.AeroStructures.Laminate | inline |
IsUsingPlyMaterials(out bool[] usingPlyMaterials) | NXOpen.CAE.AeroStructures.Laminate | inline |
LamRefLoc enum name | NXOpen.CAE.AeroStructures.Laminate | |
MassDensity | NXOpen.CAE.AeroStructures.Laminate | |
MassPerUnitArea | NXOpen.CAE.AeroStructures.Laminate | |
NextSink | NXOpen.Utilities.NXRemotableObject | |
NumMaterials | NXOpen.CAE.AeroStructures.Laminate | |
NumPlies | NXOpen.CAE.AeroStructures.Laminate | |
PhysPropName | NXOpen.CAE.AeroStructures.Laminate | |
PrintLaminateInfo(bool plies, bool props, bool mats) | NXOpen.CAE.AeroStructures.Laminate | inline |
PrintTestData(String variableName) | NXOpen.TransientObject | inline |
PrintTestData(String variableName, int lineNumber) | NXOpen.TransientObject | inline |
SetBottomFiberDistance(double distance, NXOpen.Unit distanceUnit) | NXOpen.CAE.AeroStructures.LocalLaminate | inline |
SetInverted(bool inverted) | NXOpen.CAE.AeroStructures.LocalLaminate | inline |
SetLaminateAngle(double angle, NXOpen.Unit angleUnit) | NXOpen.CAE.AeroStructures.LocalLaminate | inline |
SetPlyAngle(int plyIndex, double angle, NXOpen.Unit angleUnit) | NXOpen.CAE.AeroStructures.LocalLaminate | inline |
SetPlyMaterial(int plyIndex, NXOpen.PhysicalMaterial material) | NXOpen.CAE.AeroStructures.LocalLaminate | inline |
SetPlyMaterialByName(int plyIndex, string materialName) | NXOpen.CAE.AeroStructures.LocalLaminate | inline |
SetPlyThickness(int plyIndex, double thickness, NXOpen.Unit thicknessUnit) | NXOpen.CAE.AeroStructures.LocalLaminate | inline |
SetReferencePlane(NXOpen.CAE.AeroStructures.Laminate.LamRefLoc location) | NXOpen.CAE.AeroStructures.LocalLaminate | inline |
SetReferenceTemperature(double temperature, NXOpen.Unit temperatureUnit) | NXOpen.CAE.AeroStructures.LocalLaminate | inline |
SetReversed(bool reversed) | NXOpen.CAE.AeroStructures.LocalLaminate | inline |
SyncProcessMessage(IMessage msg) | NXOpen.Utilities.NXRemotableObject | inline |
ToShorthandNotation() | NXOpen.CAE.AeroStructures.Laminate | inline |
ToString() | NXOpen.TransientObject | inline |
TotalThickness | NXOpen.CAE.AeroStructures.Laminate | |