Le´vy Type Solutions for Symmetrically Laminated Rectangular Plates Using First-Order Shear Deformation Theory

DOI10.1115/1.3173104zbMath0634.73052OpenAlexW2065417637MaRDI QIDQ3773477

Liviu Librescu, J. N. Reddy, Ahmed A. Khdeir

Publication date: 1987

Published in: Journal of Applied Mechanics (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1115/1.3173104

zbMATH Keywords

orthotropic platestransverse deflectionsymmetrically laminated rectangular platesstate-space conceptopposite edges simply supportedcentral normal stresscombination of free, simply supported, and clamped boundary conditionsfirst-order transverse shear deformationLévy- type solutionsremaining edges

Mathematics Subject Classification ID

Anisotropy in solid mechanics (74E10) Plates (74K20) Composite and mixture properties (74E30)

Related Items (9)

On refined theories of composite laminates ⋮ On the flexural vibrations of sandwich plates ⋮ Boundary-discontinuous Fourier analysis of simply supported cross-ply plates ⋮ A shear deformable theory of laminated composite shallow shell-type panels and their response analysis. I. Free vibration and buckling ⋮ Complex potential formalisms for bending of inhomogeneous monoclinic plates including transverse shear deformation ⋮ Lévy-type solution for buckling analysis of thick functionally graded rectangular plates based on the higher-order shear deformation plate theory ⋮ Boundary layer effects in rectangular cross-ply Levy-type plates using zigzag theory ⋮ The large rotations theory of elasto‐viscoplastic shells subjected to the dynamic and thermal loads ⋮ An analytical solution of rectangular laminated plates by higher-order theory

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