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A co-rotational 8-node assumed strain shell element for postbuckling analysis of laminated composite plates and shells

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Publication:1416820
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DOI10.1007/s00466-003-0415-6zbMath1090.74687OpenAlexW2042539152MaRDI QIDQ1416820

D. Massart

Publication date: 16 December 2003

Published in: Computational Mechanics (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1007/s00466-003-0415-6

zbMATH Keywords

PostbucklingA co-rotational 8-node assumed strain shell elementLaminated composite


Mathematics Subject Classification ID

Plates (74K20) Finite element methods applied to problems in solid mechanics (74S05) Composite and mixture properties (74E30) Bifurcation and buckling (74G60) Shells (74K25)


Related Items

Free and forced vibration analysis of laminated composite plates and shells using a 9-node assumed strain shell element, A stabilized co-rotational curved quadrilateral composite shell element



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