Using the results of Problem 2.6, determine the invariants (U_{i}) and (V_{i}) for the AS/3501 lamina, where
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Using the results of Problem 2.6, determine the invariants \(U_{i}\) and \(V_{i}\) for the AS/3501 lamina, where \(i=1,2,3,4\).
Problem 2.6
Find all components of the stiffness and compliance matrices for a specially orthotropic lamina made of AS/3501 carbon/epoxy.
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Related Book For
Principles Of Composite Material Mechanics
ISBN: 9781498720694
4th Edition
Authors: Ronald F. Gibson
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