How to determine G1z and G2z (G13, G23) for carbon fiber
enriqueng
Altair Community Member
Answers
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Hi,
4 basic composite properties (E11, E22, G12, nu12) are enough to define any composite material. Remaining 5 properties (E33, nu13, nu23, G13, G23) can be derived from certain formulae.
Example: A unidirectional composite material has the following formulae: E22 = E33, nu12 = nu13, G12 = G13 and G23 = E22 / [ 2 * (1+ nu23 )].
So, this is how HyperMesh determines the remaining properties using basic properties.
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