Article ID Journal Published Year Pages File Type
253821 Composite Structures 2008 5 Pages PDF
Abstract

The buckling of an orthotropic piezoelectric rectangular laminate with weak interfaces is investigated. The state-space formulations established directly from the three-dimensional theory of elasticity are employed. The solution is completely exact and can be used as a benchmark to clarify various plate theories or numerical methods.

Related Topics
Physical Sciences and Engineering Engineering Civil and Structural Engineering
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