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Classical laminated plate theory to calculate the effective in-plane laminate properties from the in-plane lamina properties and stacking sequence. Calculates mid-plane strains and curvatures given the applied loading. Alternatively, calculates the applied loading required to achieve specified mid-plane strains and curvatures. Finally, calculates stresses and strains in each ply in both the laminate and material coordinate systems.
Carlsson, L.A.; Adams, D.F.; Pipes, R.B. "Experimental Characterization of Advanced Composite Materials." 4th Ed. CRC Press. 2014.
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