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Finite element analysis of wrinkling membranesThe finite element analysis of wrinkling membranes was investigated. The determination of stresses and deformations within large partly wrinkled membrane surfaces is a problem of significant technical interest in such areas as conceptual design and analysis of ultra lightweight spacecraft structures. A closed-form solution to an axisymmetric problem involving partial wrinkling of an inflated shallow membrane was obtained. In particular, a membrane in the shape of a sperical annulus was considered. The outer edge of the annulus was assumed to be fixed so that no displacements occur along the outer perimeter. The inner edge is assumed to be clamped to a rigid movable plug. Solutions for the complete stress, strain, and displacement fields under the assumption of inextensional material behavior are presented for the case of pure torsional loads applied to the plug, and for the case of pure axial loads applied to the plug.
Document ID
19830027139
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Miller, R. K.
(University of Southern California Los Angeles, CA, United States)
Hedgepeth, J. M.
(Astro Research Corp. Carpinteria, Calif., United States)
Weingarten, V. I.
(University of Southern California Los Angeles, CA, United States)
Das, P.
(University of Southern California Los Angeles, CA, United States)
Kahyai, S.
(University of Southern California Los Angeles, CA, United States)
Date Acquired
September 4, 2013
Publication Date
January 1, 1982
Subject Category
Structural Mechanics
Report/Patent Number
NAS 1.26:173074
NASA-CR-173074
Report Number: NAS 1.26:173074
Report Number: NASA-CR-173074
Accession Number
83N35410
Funding Number(s)
CONTRACT_GRANT: NAG1-235
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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