A consistent refined theory for flexure of a symmetric laminate

DOI10.1016/0093-6413(87)90026-7zbMath0617.73061OpenAlexW2139042551MaRDI QIDQ1822552

Tarun Kant, B. N. Pandya

Publication date: 1987

Published in: Mechanics Research Communications (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1016/0093-6413(87)90026-7

zbMATH Keywords

laminatestransverse normal stresszero transverse shear stress conditionsC (sup 0)-finite displacement elementparabolic variation of transverse shear strains/stressessandwiched platestop and bottom faces

Mathematics Subject Classification ID

Plates (74K20) Finite element methods applied to problems in solid mechanics (74S05) Composite and mixture properties (74E30)

Related Items (4)

A single variable refined theory for free vibrations of a plate using inertia related terms in displacements ⋮ Postbuckling analysis of stiffened laminated composite panels, using a higher-order shear deformation theory ⋮ Stress analyses of laminates under cylindrical bending ⋮ Predictor-corrector procedures for stress and free vibration analyses of multilayered composite plates and shells

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