A finite element-difference computational model for stress analysis of layered composite cylindrical shells

DOI10.1016/0168-874X(93)90078-5zbMath0788.73068OpenAlexW2123905704MaRDI QIDQ1309566

M. P. Menon, Tarun Kant

Publication date: 26 May 1994

Published in: Finite Elements in Analysis and Design (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1016/0168-874x(93)90078-5

zbMATH Keywords

thin shellsinterlaminar and transverse stressesLagrangian quadrilateralstangential displacementthick composite shells

Mathematics Subject Classification ID

Finite element methods applied to problems in solid mechanics (74S05) Composite and mixture properties (74E30) Finite difference methods applied to problems in solid mechanics (74S20) Membranes (74K15)

Related Items (2)

Boundary-layer hygrothermal stresses in laminated, composite, circular, cylindrical shell panels ⋮ Finite element linear and nonlinear, static and dynamic analysis of structural elements: a bibliography (1992‐1995)

This page was built for publication: A finite element-difference computational model for stress analysis of layered composite cylindrical shells