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Hadian, Mohammad Jafar
Hamilton's principle and a third-order shear-deformation theory are used to derive a set of five coupled partial-differential equations governing the nonlinear response of composite plates. The reduction of these equations by using classical plate th
Externí odkaz:
http://hdl.handle.net/10919/39785
http://scholar.lib.vt.edu/theses/available/etd-10122005-134444/
http://scholar.lib.vt.edu/theses/available/etd-10122005-134444/
