A numerical and experimental investigation of the buckling behavior of composite panels

DOI10.1016/0045-7949(82)90073-6zbMath0488.73085OpenAlexW2052693147MaRDI QIDQ3950109

N. S. Khot, Nelson R. jun. Bauld

Publication date: 1982

Published in: Computers & Structures (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1016/0045-7949(82)90073-6

zbMATH Keywords

axially compressed, fiber-reinforced, circular cylindrical panelsclamped along curved edgesenergy-based, finite difference, computer programexperimental and numerical buckling behaviorsperfect cylindrical geometrysmall axially symmetric initial imperfectionstest specimensunsupported or simply supported along straight edges

Mathematics Subject Classification ID

Experimental work for problems pertaining to mechanics of deformable solids (74-05) Composite and mixture properties (74E30) Bifurcation and buckling (74G60)

Related Items (2)

Initial post-buckling of variable-stiffness curved panels ⋮ Optimization of composite, stiffened, imperfect panels under combined loads for service in the postbuckling regime

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