Refined unified formulation for efficient folding and unfolding analyses of slender thin-walled structures
File(s)RUN___AIAA___Revision.pdf (3.01 MB)
Accepted version
Author(s)
Soltani, Zahra
Santer, Matthew
Type
Journal Article
Abstract
We present a high-fidelity refined unified nonlinear finite element formulation for the efficient and robust analysis of slender thin-walled bodies during highly nonlinear deformation. Our formulation utilizes an independent discretization of the displacement field along the beam axis and over the cross section. By matching different refinements in different cross sections, it is able to apply higher-order beam theories in highly deformed regions, to capture complex buckling and postbuckling behavior, whilst retaining the computational efficiency offered by lower refinements elsewhere. The exemplar structure for this paper is the tape spring—a commonly proposed component of deployable structures with ability to combine self-deployment, via a release of stored strain energy, with locking into a relatively stiff geometric configuration with a curved cross section. To simulate localized folds due to a flattening of the cross section, the arc-length method with an automatic increment technique is employed.
Date Issued
2022-09-01
Date Acceptance
2022-05-03
Citation
AIAA Journal: devoted to aerospace research and development, 2022, 60 (9)
ISSN
0001-1452
Publisher
American Institute of Aeronautics and Astronautics
Journal / Book Title
AIAA Journal: devoted to aerospace research and development
Volume
60
Issue
9
Copyright Statement
Copyright © 2022 by the American Institute of Aeronautics and Astronautics, Inc. All rights reserved. All requests for copying and permission to reprint should be submitted to CCC at www.copyright.com; employ the eISSN 1533-385X to initiate your request. See also AIAA Rights and Permissions www.aiaa.org/randp.
Identifier
http://gateway.webofknowledge.com/gateway/Gateway.cgi?GWVersion=2&SrcApp=PARTNER_APP&SrcAuth=LinksAMR&KeyUT=WOS:000808267700001&DestLinkType=FullRecord&DestApp=ALL_WOS&UsrCustomerID=1ba7043ffcc86c417c072aa74d649202
Subjects
Engineering
Engineering, Aerospace
Science & Technology
Technology
Publication Status
Published
Date Publish Online
2022-06-09