NDLI: Shear-flexible finite-element models of laminated composite plates and shells

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Shear-flexible finite-element models of laminated composite plates and shells

Content Provider	NASA Technical Reports Server (NTRS)
Author	Noor, A. K. Mathers, M. D.
Copyright Year	1975
Description	Several finite-element models are applied to the linear static, stability, and vibration analysis of laminated composite plates and shells. The study is based on linear shallow-shell theory, with the effects of shear deformation, anisotropic material behavior, and bending-extensional coupling included. Both stiffness (displacement) and mixed finite-element models are considered. Discussion is focused on the effects of shear deformation and anisotropic material behavior on the accuracy and convergence of different finite-element models. Numerical studies are presented which show the effects of increasing the order of the approximating polynomials, adding internal degrees of freedom, and using derivatives of generalized displacements as nodal parameters.
File Size	3328441
Page Count	115
File Format	PDF
Alternate Webpage(s)	http://archive.org/details/NASA_NTRS_Archive_19760007434
Archival Resource Key	ark:/13960/t88h3d829
Language	English
Publisher Date	1975-12-01
Access Restriction	Open
Subject Keyword	Structural Mechanics Cylindrical Shells Finite Element Method Stress Analysis Numerical Analysis Plates Structural Members Anisotropy Shear Stress Spherical Shells Laminates Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science
Content Type	Text
Resource Type	Technical Report

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