Package | Description |
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nxopen.cae.aerostructures.author |
Provides classes and interfaces relating to Aero Structures Author.
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Modifier and Type | Method and Description |
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ABB.MsTsaiHillPlaneStressData |
ABB.msTsaiHillPlaneStress(double matFcL,
double matFcLT,
double matFtL,
double matFtLT,
double matFS,
double[] fl,
double[] flt,
double[] fs)
MS Tsai-Hill
Computes margin of safety on the basis of Tsai-Hill failure theory (plane stresses hypothesis)
The formula based on yield material allowables is 'MS=1-sqrt(((F_L)/FtcyL)^2+(FLT/FtcyLT)^2-((F_LF_(LT))/(FtcyLFtcyL))+(F_(S)/Fsy)^2)'
where:
L and LT are material directions: 'Longitudinal' and 'Longitudinal' 'Transverse'.
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