Analysis of laminated bimodulus composite thin shells of revolution using a doubly curved quadrilateral finite element

DOI10.1002/NME.1620210207zbMATH Open0552.73058OpenAlexW2169821553MaRDI QIDQ3345893

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Publication date: 1985

Published in: International Journal for Numerical Methods in Engineering (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1002/nme.1620210207

zbMATH Keywords

three displacements48 degrees of freedom doubly curved quadrilateral finite elementlaminated bimodulus composite thin shells of revolutionproducts of one-dimensional first-order Hermite interpolation polynomialsshell element reference surface

Mathematics Subject Classification ID

Anisotropy in solid mechanics (74E10) Finite element methods applied to problems in solid mechanics (74S05) Composite and mixture properties (74E30) Membranes (74K15) Numerical and other methods in solid mechanics (74S99)

Related Items (2)

An efficient through-thickness integration scheme in an unlimited layer doubly curved isoparametric composite shell element ⋮ Retracted article: Free vibrations of laminated composite doubly-curved shells and panels of revolution via the GDQ method

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