2012
DOI: 10.1007/s00707-012-0774-1
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Flexural analysis of cross-ply laminated plates subjected to nonlinear thermal and mechanical loadings

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Cited by 15 publications
(6 citation statements)
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“…The MFC integrated plate structure can be treated as a laminated plate attached to MFC. TSDT are adopted by the [33,34] to obtain that the deflection and axial displacement in the xy plane of the plate structure is almost equal to that of the plate structure obtained by CPT, so CPT is adopted to obtain the plate structure curvature and axial strain [17], which is then substituted into the axial displacement formula of TSDT (4) to provide the strains ε px,c and ε py,c along the x and y axes at the midcourt line on the upper surface of the MFC:…”
Section: Mfc Actuating Force Formula Based On Tsdtmentioning
confidence: 99%
“…The MFC integrated plate structure can be treated as a laminated plate attached to MFC. TSDT are adopted by the [33,34] to obtain that the deflection and axial displacement in the xy plane of the plate structure is almost equal to that of the plate structure obtained by CPT, so CPT is adopted to obtain the plate structure curvature and axial strain [17], which is then substituted into the axial displacement formula of TSDT (4) to provide the strains ε px,c and ε py,c along the x and y axes at the midcourt line on the upper surface of the MFC:…”
Section: Mfc Actuating Force Formula Based On Tsdtmentioning
confidence: 99%
“…The actuating force caused by the deformations will be transmitted through the layer sticking up between the MFC and the plate. To consider the influence of the shear deformation of the MFC laminated plate on the MFC actuating force, SSDT [32] is adopted to deduce the MFC actuating force formula. Considering that differences exist in material parameters between the MFC and the plate, deformation compatibility and stress balance should be ensured between them, global-local displacement distribution functions are introduced to establish the stress balance equation of MFC laminated plate, and then, according to the equal shear force between the MFC and the plate, the system of stress partial differential equations is simplified and solved to obtain the interfacial shear force between the MFC and the plate structure and the actuating force and actuating bending moment of the MFC.…”
Section: The Actuating Equation Of An Mfc Laminated Plate Structurementioning
confidence: 99%
“…According to Equations (25), (26) and (30), ε px,c , ε py,c , ε px,e and ε py,e all include an influence of the piezoelectric effect in the directions of the x and y axes, and the magnitude of the interfacial shear stress τ x and τ y is related to the piezoelectric effect in the directions of the x and y axes. According to Equations (32) and (34), the total actuating forces T x and T y of the MFC at the center of the MFC laminated plate structure can be obtained:…”
Section: The Actuating Equation Of An Mfc Laminated Plate Structurementioning
confidence: 99%
“…Mechab et al [43] developed a new trigonometric shear deformation theory for the thermo-mechanical analysis of laminated composite plates. Ghugal and Kulkarni [44][45][46][47] have applied trigonometric shear deformation theory (TSDT) for the thermal analysis of cross-ply laminated plates. A higherorder shear deformation theory with Taylor series-type expansion in the thickness direction for the displacements has been developed by Kant and Khare [48] for composite and sandwich plates under thermal loading.…”
Section: Introductionmentioning
confidence: 99%