Large Deflection Behavior of Simply Supported Laminated Panels Under In-Plane Loading

DOI10.1115/1.3169100zbMath0571.73071OpenAlexW2061085122MaRDI QIDQ3687852

F. L. Matthews, Y. Zhang

Publication date: 1985

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

Full work available at URL: https://doi.org/10.1115/1.3169100

zbMATH Keywords

lateral deflectionin-plane loadingsimply supported boundariesbending effectsdifferent materialsdifferent lay-upspair of governing equationsdifferent curvaturesflat and curved panelsincreases deflectionKármán sensenonbifurcational behaviorreduces resistance against collapseunsymmetric angle-ply layers under shearunsymmetric cross-ply layers under compressionunsymmetrically laminated composite materials

Mathematics Subject Classification ID

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

Related Items (3)

Thermo-piezoelectric effects on the postbuckling of axially-loaded hybrid laminated cylindrical panels ⋮ Nonlinear bending and vibration of symmetrically laminated orthotropic elliptical plate with simply supported edge ⋮ Influence of compression-bending coupling on the stability behavior of anisotropic laminated panels

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