So far most studies use large rectangular piezoelectric macro fiber composite mfc patches bonded at the center of the laminate to induce snap through. 1a a thin 90 4 0 4 t cross ply unsymmetric graphite epoxy laminate for example will have two cylindrical configurations when cooled to room temperature. 164 and 188 the optimal stacking sequence for a 10 layer symmetric laminate is determined to be 15 30 15 0 30 s it was asserted that a multilayer composite laminate can be modeled using an equivalent unidirectional fiber angle θ eq which results in approximately the same load deformation characteristics for this particular layup the equivalent.
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