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NXOpen .NET Reference
12.0.0
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This is the complete list of members for NXOpen.CAE.AeroStructures.Author.ABB, including all inherited members.
| CurvedMetallicPanelCompressiveBucklingCoefficient(double b, double t, double r, double nu, out double kc) | NXOpen.CAE.AeroStructures.Author.ABB | |
| CurvedMetallicPanelShearBucklingCoefficient(double a, double b, double t, double r, double nu, NXOpen.CAE.AeroStructures.Author.ABB.EdgeSupportType bc, out double ks) | NXOpen.CAE.AeroStructures.Author.ABB | |
| EdgeSupportType enum name | NXOpen.CAE.AeroStructures.Author.ABB | |
| EquivalentSectionProperties(double[] n, double[] iAi, double[] iEi, double[] iIxxi, out double[] a, out double[] e, out double[] oYcog, out double[] oIxx) | NXOpen.CAE.AeroStructures.Author.ABB | |
| ExtrudedMetallicSubSectionCripplingAllowable(double iFcy, double e, int fe, double b, double t, out double iFcc) | NXOpen.CAE.AeroStructures.Author.ABB | |
| FlatMetallicPanelBendingBucklingCoefficient(double aOverB, double beta, out double kb) | NXOpen.CAE.AeroStructures.Author.ABB | |
| FlatMetallicPanelCompressiveBucklingCoefficient(double a, double b, NXOpen.CAE.AeroStructures.Author.ABB.UnloadedEdgeSupportType bcUnloaded, NXOpen.CAE.AeroStructures.Author.ABB.EdgeSupportType bcLoaded, out double kc) | NXOpen.CAE.AeroStructures.Author.ABB | |
| FlatMetallicPanelShearBucklingCoefficient(double a, double b, NXOpen.CAE.AeroStructures.Author.ABB.EdgeSupportType bc, out double ks) | NXOpen.CAE.AeroStructures.Author.ABB | |
| GetABB(NXOpen.Session owner) | NXOpen.CAE.AeroStructures.Author.ABB | static |
| GetIntegerNa() | NXOpen.CAE.AeroStructures.Author.ABB | |
| GetMsThreshold() | NXOpen.CAE.AeroStructures.Author.ABB | |
| GetPi() | NXOpen.CAE.AeroStructures.Author.ABB | |
| GetRealEpsilon() | NXOpen.CAE.AeroStructures.Author.ABB | |
| GetRealMax() | NXOpen.CAE.AeroStructures.Author.ABB | |
| GetRealNa() | NXOpen.CAE.AeroStructures.Author.ABB | |
| GetRealNegativeInfinity() | NXOpen.CAE.AeroStructures.Author.ABB | |
| GetRealPositiveInfinity() | NXOpen.CAE.AeroStructures.Author.ABB | |
| GetUltimateLimitFactor() | NXOpen.CAE.AeroStructures.Author.ABB | |
| IsRealNa(double value) | NXOpen.CAE.AeroStructures.Author.ABB | |
| IsRealNegativeInfinity(double value) | NXOpen.CAE.AeroStructures.Author.ABB | |
| IsRealPositiveInfinity(double value) | NXOpen.CAE.AeroStructures.Author.ABB | |
| LoadDistributionBoltsConcentricLoads(double[] p, double[] iPsn, int nblcXnbbolt, out double[] oPn) | NXOpen.CAE.AeroStructures.Author.ABB | |
| MaterialBehaviour enum name | NXOpen.CAE.AeroStructures.Author.ABB | |
| MaterialFsyEstimation(double iFtyL, double iFtyLT, double iFcyL, double iFcyLT, double iFsu, double iFtuL, double iFtuLT, out double oFsy) | NXOpen.CAE.AeroStructures.Author.ABB | |
| MetallicPanelCompressivePlasticityCurveBc1(double x, double n, out double z) | NXOpen.CAE.AeroStructures.Author.ABB | |
| MetallicPanelCompressivePlasticityCurveBc2(double x, double n, out double z) | NXOpen.CAE.AeroStructures.Author.ABB | |
| MetallicPanelCompressivePlasticityCurveBc3(double x, double n, out double z) | NXOpen.CAE.AeroStructures.Author.ABB | |
| MsAllowable(double allowable, double[] value, out double[] ms) | NXOpen.CAE.AeroStructures.Author.ABB | |
| MsBearing(double iFbr, double d, double t, double factor, double[] iPy, double[] iPz, out double[] ms) | NXOpen.CAE.AeroStructures.Author.ABB | |
| MsBoltBending(double iMba, double b, double factor, double[] iPy, double[] iPz, out double[] ms) | NXOpen.CAE.AeroStructures.Author.ABB | |
| MsBoltCombinedShearTension(double iPTensileAllowable, double[] iPTensileX, double iPShearAllowable, double factor, double[] iPy, double[] iPz, out double[] ms) | NXOpen.CAE.AeroStructures.Author.ABB | |
| MsBoltCombinedShearTensionBending(double iPTensileAllowable, double[] iPTensileX, double iMAllowable, double b, double factorBend, double[] iPyBend, double[] iPzBend, double iPShearAllowable, double factorShear, double[] iPyShear, double[] iPzShear, out double[] ms) | NXOpen.CAE.AeroStructures.Author.ABB | |
| MsBoltShear(double iPShearAllowable, double factor, double[] iPy, double[] iPz, out double[] ms) | NXOpen.CAE.AeroStructures.Author.ABB | |
| MsMaterialStressAllowable(double allowable, double[] sigma, out double[] ms) | NXOpen.CAE.AeroStructures.Author.ABB | |
| MsNetSection(double sigmaAllowable, double d, double t, double b, double factor, double[] iPExtracted, out double[] ms) | NXOpen.CAE.AeroStructures.Author.ABB | |
| MsPlateBuckling(double e, double nu, double b, double t, double k, double eta, double[] sigma, out double[] ms) | NXOpen.CAE.AeroStructures.Author.ABB | |
| MsPlateBucklingCurvedCompressive(double e, double nu, double n, double a, double b, double t, double r, NXOpen.CAE.AeroStructures.Author.ABB.MaterialBehaviour behaviour, double[] sigma, out double[] ms, out double sigmaAllowable) | NXOpen.CAE.AeroStructures.Author.ABB | |
| MsPlateBucklingCurvedLongitudinalShearCombined(double e, double nu, double n, double a, double b, double t, NXOpen.CAE.AeroStructures.Author.ABB.EdgeSupportType bc, double r, NXOpen.CAE.AeroStructures.Author.ABB.MaterialBehaviour behaviour, double[] sigma, double[] tau, out double[] ms, out double sigmacr, out double taucr) | NXOpen.CAE.AeroStructures.Author.ABB | |
| MsPlateBucklingCurvedShear(double e, double nu, double n, double a, double b, double t, NXOpen.CAE.AeroStructures.Author.ABB.EdgeSupportType bc, double r, NXOpen.CAE.AeroStructures.Author.ABB.MaterialBehaviour behaviour, double[] sigma, out double[] ms, out double sigmaAllowable) | NXOpen.CAE.AeroStructures.Author.ABB | |
| MsPlateBucklingFlatBending(double e, double nu, double n, double a, double b, double beta, double t, NXOpen.CAE.AeroStructures.Author.ABB.MaterialBehaviour behaviour, double[] sigma1, double[] sigma2, out double[] ms, out double[] sigmaAllowable) | NXOpen.CAE.AeroStructures.Author.ABB | |
| MsPlateBucklingFlatCompressive(double e, double nu, double n, double a, double b, double t, NXOpen.CAE.AeroStructures.Author.ABB.UnloadedEdgeSupportType bcUnloaded, NXOpen.CAE.AeroStructures.Author.ABB.EdgeSupportType bcLoaded, NXOpen.CAE.AeroStructures.Author.ABB.MaterialBehaviour behaviour, double[] sigma, out double[] ms, out double sigmaAllowable) | NXOpen.CAE.AeroStructures.Author.ABB | |
| MsPlateBucklingFlatLongitudinalBendingCombined(double e, double nu, double n, double a, double b, double t, NXOpen.CAE.AeroStructures.Author.ABB.UnloadedEdgeSupportType bcUnloaded, NXOpen.CAE.AeroStructures.Author.ABB.EdgeSupportType bcLoaded, NXOpen.CAE.AeroStructures.Author.ABB.MaterialBehaviour behaviour, double[] sigma1, double[] sigma2, out double[] ms, out double sigmacr, out double sigmabcr) | NXOpen.CAE.AeroStructures.Author.ABB | |
| MsPlateBucklingFlatLongitudinalShearCombined(double e, double nu, double n, double a, double b, double t, NXOpen.CAE.AeroStructures.Author.ABB.UnloadedEdgeSupportType bcUnloaded, NXOpen.CAE.AeroStructures.Author.ABB.EdgeSupportType bcLoaded, NXOpen.CAE.AeroStructures.Author.ABB.MaterialBehaviour behaviour, double[] sigma, double[] tau, out double[] ms, out double sigmacr, out double taucr) | NXOpen.CAE.AeroStructures.Author.ABB | |
| MsPlateBucklingFlatShear(double e, double nu, double n, double a, double b, double t, NXOpen.CAE.AeroStructures.Author.ABB.EdgeSupportType bc, NXOpen.CAE.AeroStructures.Author.ABB.MaterialBehaviour behaviour, double[] sigma, out double[] ms, out double sigmaAllowable) | NXOpen.CAE.AeroStructures.Author.ABB | |
| MsPlateBucklingFlatShearBendingCombined(double e, double nu, double n, double a, double b, double t, NXOpen.CAE.AeroStructures.Author.ABB.UnloadedEdgeSupportType bcUnloaded, NXOpen.CAE.AeroStructures.Author.ABB.EdgeSupportType bcLoaded, NXOpen.CAE.AeroStructures.Author.ABB.MaterialBehaviour behaviour, double[] sigma1, double[] sigma2, double[] tau, out double[] ms, out double sigmabcr, out double taucr) | NXOpen.CAE.AeroStructures.Author.ABB | |
| MsShearTearOut(double tauAllowable, double d, double t, double b, double factor, double[] iPExtracted, out double[] ms) | NXOpen.CAE.AeroStructures.Author.ABB | |
| MsTrescaPlaneStress(double fs, double[] fx, double[] fy, double[] fxy, out double[] ms) | NXOpen.CAE.AeroStructures.Author.ABB | |
| MsTsaiHillPlaneStress(double matFcL, double matFcLT, double matFtL, double matFtLT, double matFS, double[] fl, double[] flt, double[] fs, out double[] ms) | NXOpen.CAE.AeroStructures.Author.ABB | |
| SecantModulus(double e, double n, double fy, double sigma, out double iEs) | NXOpen.CAE.AeroStructures.Author.ABB | |
| Status enum name | NXOpen.CAE.AeroStructures.Author.ABB | |
| StressF07(double iFy, double e, double n, out double f07) | NXOpen.CAE.AeroStructures.Author.ABB | |
| StressFromStrainInPlasticDomain(double strain, double e, double iF02ys, double n, out double sigma) | NXOpen.CAE.AeroStructures.Author.ABB | |
| Tag | NXOpen.CAE.AeroStructures.Author.ABB | |
| TangentModulus(double e, double n, double iFy, double sigma, out double oEt) | NXOpen.CAE.AeroStructures.Author.ABB | |
| UnloadedEdgeSupportType enum name | NXOpen.CAE.AeroStructures.Author.ABB |