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Development and evaluation of two non-linear shell elementsTwo plate and shell displacement elements are developed for use in large deflection non-linear analysis. The elements are of the 'stability' type, in which non-linear strains are included, with their values optimized by added higher order membrane functions and special types of elemental level constraints. The paper summarizes formulation and computational procedures, and discusses numerical results in detail. Conclusions are given regarding the effectiveness of the elements for solving both linear and non-linear shell analysis problems.
Document ID
19810038577
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Jones, R. E.
(Boeing Aerospace Co. Seattle, WA, United States)
Vos, R. G.
(Boeing Aerospace Co. Seattle, Wash., United States)
Date Acquired
August 11, 2013
Publication Date
October 1, 1980
Publication Information
Publication: International Journal for Numerical Methods in Engineering
Volume: 16
Subject Category
Structural Mechanics
Accession Number
81A22981
Distribution Limits
Public
Copyright
Other

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