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NXOpen .NET Reference Guide
1899
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NXOpen .NET Reference Guide
1899
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This is the complete list of members for NXOpen.CAE.AeroStructures.Author.ABB, including all inherited members.
| AsyncProcessMessage(IMessage msg, IMessageSink replySink) | NXOpen.Utilities.NXRemotableObject | inline |
| CurvedMetallicPanelCompressiveBucklingCoefficient(NXOpen.CAE.AeroStructures.Author.AbbContext abbContext, double b, double t, double r, double nu, out double kc) | NXOpen.CAE.AeroStructures.Author.ABB | inline |
| CurvedMetallicPanelShearBucklingCoefficient(NXOpen.CAE.AeroStructures.Author.AbbContext abbContext, 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 | inline |
| EdgeSupportType enum name | NXOpen.CAE.AeroStructures.Author.ABB | |
| EquivalentSectionProperties(NXOpen.CAE.AeroStructures.Author.AbbContext abbContext, double[] iAi, double[] iYcog, double[] iEi, double[] iIxxi, out double[] a, out double[] oYcog, out double[] e, out double[] oIxx) | NXOpen.CAE.AeroStructures.Author.ABB | inline |
| ExtrudedMetallicSubSectionCripplingAllowable(NXOpen.CAE.AeroStructures.Author.AbbContext abbContext, double iFcy, double e, int fe, double b, double t, out double iFcc) | NXOpen.CAE.AeroStructures.Author.ABB | inline |
| FlatMetallicPanelBendingBucklingCoefficient(NXOpen.CAE.AeroStructures.Author.AbbContext abbContext, double aOverB, double beta, out double kb) | NXOpen.CAE.AeroStructures.Author.ABB | inline |
| FlatMetallicPanelCompressiveBucklingCoefficient(NXOpen.CAE.AeroStructures.Author.AbbContext abbContext, 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 | inline |
| FlatMetallicPanelShearBucklingCoefficient(NXOpen.CAE.AeroStructures.Author.AbbContext abbContext, double a, double b, NXOpen.CAE.AeroStructures.Author.ABB.EdgeSupportType bc, out double ks) | NXOpen.CAE.AeroStructures.Author.ABB | inline |
| GetABB(NXOpen.Session owner) | NXOpen.CAE.AeroStructures.Author.ABB | inlinestatic |
| GetIntegerNa() | NXOpen.CAE.AeroStructures.Author.ABB | inline |
| GetMsThreshold() | NXOpen.CAE.AeroStructures.Author.ABB | inline |
| GetPi() | NXOpen.CAE.AeroStructures.Author.ABB | inline |
| GetRealEpsilon() | NXOpen.CAE.AeroStructures.Author.ABB | inline |
| GetRealMax() | NXOpen.CAE.AeroStructures.Author.ABB | inline |
| GetRealNa() | NXOpen.CAE.AeroStructures.Author.ABB | inline |
| GetRealNegativeInfinity() | NXOpen.CAE.AeroStructures.Author.ABB | inline |
| GetRealPositiveInfinity() | NXOpen.CAE.AeroStructures.Author.ABB | inline |
| GetUltimateLimitFactor() | NXOpen.CAE.AeroStructures.Author.ABB | inline |
| IsRealNa(double value) | NXOpen.CAE.AeroStructures.Author.ABB | inline |
| IsRealNegativeInfinity(double value) | NXOpen.CAE.AeroStructures.Author.ABB | inline |
| IsRealPositiveInfinity(double value) | NXOpen.CAE.AeroStructures.Author.ABB | inline |
| LoadDistributionBoltsConcentricLoads(NXOpen.CAE.AeroStructures.Author.AbbContext abbContext, double[] p, double[] iPsn, out double[] oPn) | NXOpen.CAE.AeroStructures.Author.ABB | inline |
| MaterialBehaviour enum name | NXOpen.CAE.AeroStructures.Author.ABB | |
| MaterialFsyEstimation(NXOpen.CAE.AeroStructures.Author.AbbContext abbContext, double iFtyL, double iFtyLT, double iFcyL, double iFcyLT, double iFsu, double iFtuL, double iFtuLT, out double oFsy) | NXOpen.CAE.AeroStructures.Author.ABB | inline |
| MetallicPanelCompressivePlasticityCurveBc1(NXOpen.CAE.AeroStructures.Author.AbbContext abbContext, double x, double n, out double z) | NXOpen.CAE.AeroStructures.Author.ABB | inline |
| MetallicPanelCompressivePlasticityCurveBc2(NXOpen.CAE.AeroStructures.Author.AbbContext abbContext, double x, double n, out double z) | NXOpen.CAE.AeroStructures.Author.ABB | inline |
| MetallicPanelCompressivePlasticityCurveBc3(NXOpen.CAE.AeroStructures.Author.AbbContext abbContext, double x, double n, out double z) | NXOpen.CAE.AeroStructures.Author.ABB | inline |
| MsAllowable(NXOpen.CAE.AeroStructures.Author.AbbContext abbContext, double allowable, double[] value, out double[] ms) | NXOpen.CAE.AeroStructures.Author.ABB | inline |
| MsBearing(NXOpen.CAE.AeroStructures.Author.AbbContext abbContext, double d, double t, double iFbr, double f, double[] p, out double[] ms) | NXOpen.CAE.AeroStructures.Author.ABB | inline |
| MsBoltBending(NXOpen.CAE.AeroStructures.Author.AbbContext abbContext, double b, double iMba, double f, double[] p, out double[] ms) | NXOpen.CAE.AeroStructures.Author.ABB | inline |
| MsBoltCombinedShearTension(NXOpen.CAE.AeroStructures.Author.AbbContext abbContext, double iPtx, double iPss, double[] iPx, double f, double[] p, out double[] ms) | NXOpen.CAE.AeroStructures.Author.ABB | inline |
| MsBoltCombinedShearTensionBending(NXOpen.CAE.AeroStructures.Author.AbbContext abbContext, double b, double iMba, double iPtx, double iPss, double fb, double[] iPb, double[] iPx, double fs, double[] iPs, out double[] ms) | NXOpen.CAE.AeroStructures.Author.ABB | inline |
| MsBoltShear(NXOpen.CAE.AeroStructures.Author.AbbContext abbContext, double iPss, double f, double[] p, out double[] ms) | NXOpen.CAE.AeroStructures.Author.ABB | inline |
| MsColumnEccentricLoadSecantFormula(NXOpen.CAE.AeroStructures.Author.AbbContext abbContext, double a, double l, double e, double i, double sigmacr, double c, double ecc, double extrmfbrdist, double[] sigma, out double iPcr, out double[] ms) | NXOpen.CAE.AeroStructures.Author.ABB | inline |
| MsColumnEngesser(NXOpen.CAE.AeroStructures.Author.AbbContext abbContext, double a, double l, double e, double i, double n, double iFy, double c, double[] sigma, out double sigmacr, out double[] ms) | NXOpen.CAE.AeroStructures.Author.ABB | inline |
| MsColumnEuler(NXOpen.CAE.AeroStructures.Author.AbbContext abbContext, double a, double l, double e, double i, double c, double[] sigma, out double sigmacr, out double[] ms) | NXOpen.CAE.AeroStructures.Author.ABB | inline |
| MsColumnJohnsonEuler(NXOpen.CAE.AeroStructures.Author.AbbContext abbContext, double a, double l, double i, double e, double c, double sigma0, double[] sigma, out double sigmacr, out double[] ms) | NXOpen.CAE.AeroStructures.Author.ABB | inline |
| MsColumnTorsionalbuckling(NXOpen.CAE.AeroStructures.Author.AbbContext abbContext, double l, double e, double g, double j, double gamma, double r0, double c, double[] load, out double iPcr, out double[] ms) | NXOpen.CAE.AeroStructures.Author.ABB | inline |
| MsCompositePlateBucklingFlatCompressive(NXOpen.CAE.AeroStructures.Author.AbbContext abbContext, double b, double a, NXOpen.CAE.AeroStructures.Author.ABB.PlaneStressBoundaryConditions bc, NXOpen.CAE.AeroStructures.Laminate laminate, double[] sigma, out double[] ms, out double sigmaAllowable) | NXOpen.CAE.AeroStructures.Author.ABB | inline |
| MsCompositePlateBucklingFlatLongitudinalShearCombined(NXOpen.CAE.AeroStructures.Author.AbbContext abbContext, double b, double a, NXOpen.CAE.AeroStructures.Author.ABB.PlaneStressBoundaryConditions bc, NXOpen.CAE.AeroStructures.Laminate laminate, double[] sigma, double[] tau, out double[] ms, out double sigmaAllowable, out double tauAllowable) | NXOpen.CAE.AeroStructures.Author.ABB | inline |
| MsCompositePlateBucklingFlatShear(NXOpen.CAE.AeroStructures.Author.AbbContext abbContext, double b, double a, NXOpen.CAE.AeroStructures.Author.ABB.PlaneStressBoundaryConditions bc, NXOpen.CAE.AeroStructures.Laminate laminate, double[] tau, out double[] ms, out double tauAllowable) | NXOpen.CAE.AeroStructures.Author.ABB | inline |
| MsInterrivetbucklingColumn(NXOpen.CAE.AeroStructures.Author.AbbContext abbContext, double t, double p, NXOpen.CAE.AeroStructures.Author.ABB.MaterialBehaviour behaviour, double e, double iFy, double n, double c, double[] sigma, out double[] ms) | NXOpen.CAE.AeroStructures.Author.ABB | inline |
| MsInterrivetbucklingWidecolumn(NXOpen.CAE.AeroStructures.Author.AbbContext abbContext, double t, double p, NXOpen.CAE.AeroStructures.Author.ABB.MaterialBehaviour behaviour, double e, double nu, double n, double iFy, double c, double[] sigma, out double[] ms) | NXOpen.CAE.AeroStructures.Author.ABB | inline |
| MsNetSection(NXOpen.CAE.AeroStructures.Author.AbbContext abbContext, double d, double b, double t, double iFx, double f, double[] p, out double[] ms) | NXOpen.CAE.AeroStructures.Author.ABB | inline |
| MsPlateBuckling(NXOpen.CAE.AeroStructures.Author.AbbContext abbContext, double b, double t, double e, double nu, double eta, double k, double[] sigma, out double[] ms) | NXOpen.CAE.AeroStructures.Author.ABB | inline |
| MsPlateBucklingCurvedCompressive(NXOpen.CAE.AeroStructures.Author.AbbContext abbContext, double b, double a, double t, double r, NXOpen.CAE.AeroStructures.Author.ABB.MaterialBehaviour behaviour, double e, double nu, double n, double iFy, double[] sigma, out double[] ms, out double sigmaAllowable) | NXOpen.CAE.AeroStructures.Author.ABB | inline |
| MsPlateBucklingCurvedLongitudinalShearCombined(NXOpen.CAE.AeroStructures.Author.AbbContext abbContext, double b, double a, NXOpen.CAE.AeroStructures.Author.ABB.EdgeSupportType bc, double t, double r, NXOpen.CAE.AeroStructures.Author.ABB.MaterialBehaviour behaviour, double e, double nu, double n, double iFy, double[] sigma, double[] tau, out double[] ms, out double sigmacr, out double taucr) | NXOpen.CAE.AeroStructures.Author.ABB | inline |
| MsPlateBucklingCurvedShear(NXOpen.CAE.AeroStructures.Author.AbbContext abbContext, double b, double a, NXOpen.CAE.AeroStructures.Author.ABB.EdgeSupportType bc, double t, double r, NXOpen.CAE.AeroStructures.Author.ABB.MaterialBehaviour behaviour, double e, double nu, double n, double iFy, double[] tau, out double[] ms, out double tauAllowable) | NXOpen.CAE.AeroStructures.Author.ABB | inline |
| MsPlateBucklingFlatBending(NXOpen.CAE.AeroStructures.Author.AbbContext abbContext, double b, double a, double t, NXOpen.CAE.AeroStructures.Author.ABB.MaterialBehaviour behaviour, double e, double nu, double n, double iFy, double beta, double[] sigma1, double[] sigma2, out double[] ms, out double[] sigmaAllowable) | NXOpen.CAE.AeroStructures.Author.ABB | inline |
| MsPlateBucklingFlatCompressive(NXOpen.CAE.AeroStructures.Author.AbbContext abbContext, double b, NXOpen.CAE.AeroStructures.Author.ABB.EdgeSupportType bcLoaded, double a, NXOpen.CAE.AeroStructures.Author.ABB.UnloadedEdgeSupportType bcUnloaded, double t, NXOpen.CAE.AeroStructures.Author.ABB.MaterialBehaviour behaviour, double e, double nu, double n, double iFy, double[] sigma, out double[] ms, out double sigmaAllowable) | NXOpen.CAE.AeroStructures.Author.ABB | inline |
| MsPlateBucklingFlatLongitudinalBendingCombined(NXOpen.CAE.AeroStructures.Author.AbbContext abbContext, double b, NXOpen.CAE.AeroStructures.Author.ABB.EdgeSupportType bcLoaded, double a, NXOpen.CAE.AeroStructures.Author.ABB.UnloadedEdgeSupportType bcUnloaded, double t, NXOpen.CAE.AeroStructures.Author.ABB.MaterialBehaviour behaviour, double e, double nu, double n, double iFy, double[] sigma1, double[] sigma2, out double[] ms, out double sigmacr, out double sigmabcr) | NXOpen.CAE.AeroStructures.Author.ABB | inline |
| MsPlateBucklingFlatLongitudinalShearCombined(NXOpen.CAE.AeroStructures.Author.AbbContext abbContext, double b, NXOpen.CAE.AeroStructures.Author.ABB.EdgeSupportType bcLoaded, double a, NXOpen.CAE.AeroStructures.Author.ABB.UnloadedEdgeSupportType bcUnloaded, double t, NXOpen.CAE.AeroStructures.Author.ABB.MaterialBehaviour behaviour, double e, double nu, double n, double iFy, double[] sigma, double[] tau, out double[] ms, out double sigmacr, out double taucr) | NXOpen.CAE.AeroStructures.Author.ABB | inline |
| MsPlateBucklingFlatShear(NXOpen.CAE.AeroStructures.Author.AbbContext abbContext, double b, double a, NXOpen.CAE.AeroStructures.Author.ABB.EdgeSupportType bc, double t, NXOpen.CAE.AeroStructures.Author.ABB.MaterialBehaviour behaviour, double e, double nu, double n, double iFy, double[] tau, out double[] ms, out double tauAllowable) | NXOpen.CAE.AeroStructures.Author.ABB | inline |
| MsPlateBucklingFlatShearBendingCombined(NXOpen.CAE.AeroStructures.Author.AbbContext abbContext, double b, NXOpen.CAE.AeroStructures.Author.ABB.EdgeSupportType bcLoaded, double a, NXOpen.CAE.AeroStructures.Author.ABB.UnloadedEdgeSupportType bcUnloaded, double t, NXOpen.CAE.AeroStructures.Author.ABB.MaterialBehaviour behaviour, double e, double nu, double n, double iFy, double[] sigma1, double[] sigma2, double[] tau, out double[] ms, out double[] sigmabcr, out double taucr) | NXOpen.CAE.AeroStructures.Author.ABB | inline |
| MsShearTearOut(NXOpen.CAE.AeroStructures.Author.AbbContext abbContext, double d, double b, double t, double iFs, double f, double[] p, out double[] ms) | NXOpen.CAE.AeroStructures.Author.ABB | inline |
| MsTrescaPlaneStress(NXOpen.CAE.AeroStructures.Author.AbbContext abbContext, double iSTresca, double[] iFx, double[] iFy, double[] iFxy, out double[] ms) | NXOpen.CAE.AeroStructures.Author.ABB | inline |
| MsTsaiHillPlaneStress(NXOpen.CAE.AeroStructures.Author.AbbContext abbContext, double iXt, double iXc, double iYt, double iYc, double s, double[] sigma1, double[] sigma2, double[] tau, out double[] ms) | NXOpen.CAE.AeroStructures.Author.ABB | inline |
| NextSink | NXOpen.Utilities.NXRemotableObject | |
| PlaneStressBoundaryConditions enum name | NXOpen.CAE.AeroStructures.Author.ABB | |
| SecantModulus(NXOpen.CAE.AeroStructures.Author.AbbContext abbContext, double e, double n, double fy, double sigma, out double iEs) | NXOpen.CAE.AeroStructures.Author.ABB | inline |
| Status enum name | NXOpen.CAE.AeroStructures.Author.ABB | |
| StressF07(NXOpen.CAE.AeroStructures.Author.AbbContext abbContext, double iFy, double e, double n, out double f07) | NXOpen.CAE.AeroStructures.Author.ABB | inline |
| StressFromStrainInPlasticDomain(NXOpen.CAE.AeroStructures.Author.AbbContext abbContext, double strain, double e, double iF02ys, double n, out double sigma) | NXOpen.CAE.AeroStructures.Author.ABB | inline |
| SyncProcessMessage(IMessage msg) | NXOpen.Utilities.NXRemotableObject | inline |
| Tag | NXOpen.CAE.AeroStructures.Author.ABB | |
| TangentModulus(NXOpen.CAE.AeroStructures.Author.AbbContext abbContext, double e, double n, double iFy, double sigma, out double oEt) | NXOpen.CAE.AeroStructures.Author.ABB | inline |
| UnloadedEdgeSupportType enum name | NXOpen.CAE.AeroStructures.Author.ABB |
