| AsyncProcessMessage(IMessage msg, IMessageSink replySink) | NXOpen.Utilities.NXRemotableObject | inline |
| CreateLocalLaminateByCopy() | NXOpen.CAE.AeroStructures.Laminate | inline |
| Dispose() | NXOpen.TransientObject | inline |
| FreeResource() | NXOpen.CAE.AeroStructures.Laminate | 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 |
| SyncProcessMessage(IMessage msg) | NXOpen.Utilities.NXRemotableObject | inline |
| ToShorthandNotation() | NXOpen.CAE.AeroStructures.Laminate | inline |
| ToString() | NXOpen.TransientObject | inline |
| TotalThickness | NXOpen.CAE.AeroStructures.Laminate | |
