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.MsBearingData |
ABB.msBearing(double iFbr,
double d,
double t,
double factor,
double[] iPy,
double[] iPz)
MS bearing
Computes margin of bearing
The formula is 'MS = PBearingAllowable / P - 1'
where
'PBearingAllowable' is the bearing load allowable ('PBearingAllowable = Fbr * D * t')
'Fbr' is the bearing stress allowable
'D' is the d iameter
't' is the thickness
'P' is the bearing load (P = FactorLoad * PExtracted)
'FactorLoad' is the ratio of load between extracted load 'PExtracted' and 'P'
'PExtracted' is the extracted load ('PExtracted = sqrt( Py ^ 2 + Pz ^ 2 )')
'Py' is the shear load in Y direction
'Pz' is the shear load in Z direction
Input
Fbr Bearing stress allowable
D Diameter
t Thickness
Factor Load factor
Py Shear load Y direction
Pz Shear load Z direction
Output
MS Margin of safety
Return
Status of the calculation
License requirements: nx_masterfem ("Finite Element Modeling") . |
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