This research presents the modeling and analysis for the buckling and postbuckling behavior of sandwich plates under thermal and mechanical loads. The lay-up configurations of plates are laminated composite with concentric stiffener and surface mounted piezoelectric actuators. The plates are in contact with a three-parameter elastic foundation including softening and/or hardening nonlinearity. Several types of grid shapes of stiffeners are studied such as ortho grid, angle grid, iso grid, and orthotropic grid. The equations of structures are formulated based on the classical lamination theory incorporating nonlinear von-Karman relationships. The stress function and Galerkin procedure are applied to derive explicit formulations of the equilibrium paths. New results are introduced to give the influences of voltage through the thickness of piezoelectric actuators, different stiffeners, and nonlinear elastic foundations.
机构:
Univ Tehran, Fac New Sci & Technol, POB 14395-1561, Tehran 1439957131, IranUniv Tehran, Fac New Sci & Technol, POB 14395-1561, Tehran 1439957131, Iran
Bohlooly, Mehdi
Mirzavand, Babak
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Univ Tehran, Fac New Sci & Technol, POB 14395-1561, Tehran 1439957131, IranUniv Tehran, Fac New Sci & Technol, POB 14395-1561, Tehran 1439957131, Iran
机构:
Shanghai Jiao Tong Univ, Sch Aeronaut & Astronaut, Shanghai 200240, Peoples R ChinaShanghai Jiao Tong Univ, Sch Aeronaut & Astronaut, Shanghai 200240, Peoples R China
Shen, Hui-Shen
Xiang, Y.
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Western Sydney Univ, Sch Comp Engn & Math, Locked Bag 1797, Penrith, NSW 2751, Australia
Western Sydney Univ, Ctr Infrastruct Engn, Locked Bag 1797, Penrith, NSW 2751, AustraliaShanghai Jiao Tong Univ, Sch Aeronaut & Astronaut, Shanghai 200240, Peoples R China
Xiang, Y.
Lin, Feng
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Western Sydney Univ, Sch Comp Engn & Math, Locked Bag 1797, Penrith, NSW 2751, AustraliaShanghai Jiao Tong Univ, Sch Aeronaut & Astronaut, Shanghai 200240, Peoples R China