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Title: Wrinkling of composite-facing sandwich panels under biaxial loading
Author (s): Birman, Victor
Bert, Charles W.
Department/Lab Affiliations: Center for Infrastructure Engineering Studies
Engineering Education Center at St. Louis
Keywords: biaxial loading
sandwich panels
wrinkling instability
Issue Date: 2004
Publisher: SAGE Publications
Citation: Birman, Victor and Charles W. Bert “Wrinkling of Composite-Facing Sandwich Panels under Biaxial Loading”, Journal of Sandwich Structures and Materials, vol. 6, no. 3, pp. 217-237, 2004.
Abstract: The problem of face wrinkling in sandwich structures was identified as an important failure mode and first analyzed in 1940 by Gough et al. [1], who used a Winkler-type elastic foundation to model the core. This work was followed by experiments and further analysis by many others. Until 1966 all of the research was devoted to uniaxial compression loading. However, in many applications, such as naval and aircraft structures, panels are subjected to biaxial loading. Such loadings were first analyzed by Plantema in 1966 [2] for the case of sandwich constructed of isotropic materials. Sullins et al. [3] suggested an interaction equation that can be used as a criterion of wrinkling under compression in the principal directions. This equation is formulated in terms of the ratios of the principal compressive stresses to the corresponding wrinkling stresses. More recently Fagerberg [4, 5] and Vonach and Rammerstorfer [6] considered the case of sandwich with orthotropic facings. The present work attacks the subject problem using three different models for the core. One model uses a simple Winkler elastic foundation approach. The second model, following Hoff and Mautner [Hoff, N.J. and Mautner, S.E. (1945). The Buckling of Sandwich-Type Panels, Journal of the Aeronautical Sciences, 12: 285–297.], uses a linear model for the decay in deformation from the core-facing interface, while the third model, following Plantema [Plantema, F.J. (1966). Sandwich Construction, John Wiley & Sons, Inc., New York.], uses an exponential decay.
Type: Article - Journal
text
In Title: Journal of Sandwich Structures and Materials
Copyright Notice: This material is presented to ensure timely dissemination of scholarly and technical work. Copyright and all rights therein are retained by authors or by other copyright holders. All persons copying this information are expected to adhere to the terms and constraints invoked by each author's copyright. In most cases, these works may not be reposted without the explicit permission of the copyright holder.
Pre-print: author can archive; Post-print: author can archive with restrictions;Restriction: 12 month embargo; Conditions: Authors are required to contact publisher before posting (permissions below will always be granted);On author or institutional server and PubMed Central;On authors personal web site;Publisher copyright and source must be acknowledged;Publishers PDF cannot be used;Post-print version with changes from referees comments can be used;"as published" final version with layout and copy-editing changes cannot be archived but can be used on secure institutional intranet;If funding agency rules apply, authors may use SAGE open to comply;
FULL COPYRIGHT INFORMATION:
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Publisher URL:
http://dx.doi.org/10.1177/1099636204033643
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titleWrinkling of composite-facing sandwich panels under biaxial loading
contributor.authorBirman, Victor
contributor.authorBert, Charles W.
contributor.deptlabCenter for Infrastructure Engineering Studies
contributor.deptlabEngineering Education Center at St. Louis
subjectbiaxial loading
subjectsandwich panels
subjectwrinkling instability
date.issued2004
publisherSAGE Publications
identifier.citationBirman, Victor and Charles W. Bert “Wrinkling of Composite-Facing Sandwich Panels under Biaxial Loading”, Journal of Sandwich Structures and Materials, vol. 6, no. 3, pp. 217-237, 2004.
identifier.pub.URI
http://dx.doi.org/10.1177/1099636204033643
description.abstractThe problem of face wrinkling in sandwich structures was identified as an important failure mode and first analyzed in 1940 by Gough et al. [1], who used a Winkler-type elastic foundation to model the core. This work was followed by experiments and further analysis by many others. Until 1966 all of the research was devoted to uniaxial compression loading. However, in many applications, such as naval and aircraft structures, panels are subjected to biaxial loading. Such loadings were first analyzed by Plantema in 1966 [2] for the case of sandwich constructed of isotropic materials. Sullins et al. [3] suggested an interaction equation that can be used as a criterion of wrinkling under compression in the principal directions. This equation is formulated in terms of the ratios of the principal compressive stresses to the corresponding wrinkling stresses. More recently Fagerberg [4, 5] and Vonach and Rammerstorfer [6] considered the case of sandwich with orthotropic facings. The present work attacks the subject problem using three different models for the core. One model uses a simple Winkler elastic foundation approach. The second model, following Hoff and Mautner [Hoff, N.J. and Mautner, S.E. (1945). The Buckling of Sandwich-Type Panels, Journal of the Aeronautical Sciences, 12: 285–297.], uses a linear model for the decay in deformation from the core-facing interface, while the third model, following Plantema [Plantema, F.J. (1966). Sandwich Construction, John Wiley & Sons, Inc., New York.], uses an exponential decay.
typeArticle - Journal
type.DCMITypetext
type.statusPostprint
rightsThis material is presented to ensure timely dissemination of scholarly and technical work. Copyright and all rights therein are retained by authors or by other copyright holders. All persons copying this information are expected to adhere to the terms and constraints invoked by each author's copyright. In most cases, these works may not be reposted without the explicit permission of the copyright holder.
rightsPre-print: author can archive; Post-print: author can archive with restrictions;Restriction: 12 month embargo; Conditions: Authors are required to contact publisher before posting (permissions below will always be granted);On author or institutional server and PubMed Central;On authors personal web site;Publisher copyright and source must be acknowledged;Publishers PDF cannot be used;Post-print version with changes from referees comments can be used;"as published" final version with layout and copy-editing changes cannot be archived but can be used on secure institutional intranet;If funding agency rules apply, authors may use SAGE open to comply;
rights.URI
http://www.sagepub.co.uk/authors/journal/permissions.sp
relation.isPartOfJournal of Sandwich Structures and Materials
date.available2008-09-29T14:53:35Z
identifier.persist.URI
http://scholarsmine.mst.edu/post_prints/WrinklingOfComposite-FacingSandwichPanelsUnde_09007dcc8057d575.html