An improved plate theory of \(\{1,2\}\)-order for thick composite laminates

DOI10.1016/0020-7683(93)90022-YzbMath0804.73027OpenAlexW2009616942MaRDI QIDQ1210011

Alexander Tessler

Publication date: 16 May 1993

Published in: International Journal of Solids and Structures (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1016/0020-7683(93)90022-y

zbMATH Keywords

expansiondisplacementsfinite element approximationscylindrical bending of an infinite carbon/epoxy laminatelinear elastostatic analysisReissner's first order shear-deformation theorysinusoidal transverse pressure

Mathematics Subject Classification ID

Plates (74K20) Composite and mixture properties (74E30)

Related Items (6)

Robust C0 high-order plate finite element for thin to very thick structures: mechanical and thermo-mechanical analysis ⋮ Computational homogenisation of composite plates: consideration of the thickness change with a modified projection strategy ⋮ Refined zigzag theory for homogeneous, laminated composite, and sandwich beams derived from Reissner's mixed variational principle ⋮ Finite element linear and nonlinear, static and dynamic analysis of structural elements: a bibliography (1992‐1995) ⋮ Complete stress field in sandwich panels with a new triangular finite element of single-layer theory ⋮ A homogeneous limit methodology and refinements of computationally efficient zigzag theory for homogeneous, laminated composite, and sandwich plates

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