Loading…
Elasticity Solution for Curved Sandwich Beams/Panels and Comparison with Structural Theories
The linear elasticity problem formulation and solution for a generally asymmetric sandwich curved beam/panel consisting of orthotropic core and face sheets, which is subjected to a top face sinusoidal distributed transverse loading, is presented. The displacement approach is used along with a plane...
Saved in:
Published in: | AIAA journal 2017-09, Vol.55 (9), p.3153-3160 |
---|---|
Main Authors: | , , |
Format: | Article |
Language: | English |
Subjects: | |
Citations: | Items that this one cites Items that cite this one |
Online Access: | Get full text |
Tags: |
Add Tag
No Tags, Be the first to tag this record!
|
cited_by | cdi_FETCH-LOGICAL-a351t-c456d1a6fe4eb320f8e22d5572293dacd9df69b92199afc6ddb5d2323045b0b73 |
---|---|
cites | cdi_FETCH-LOGICAL-a351t-c456d1a6fe4eb320f8e22d5572293dacd9df69b92199afc6ddb5d2323045b0b73 |
container_end_page | 3160 |
container_issue | 9 |
container_start_page | 3153 |
container_title | AIAA journal |
container_volume | 55 |
creator | Kardomateas, George A Rodcheuy, Nunthadech Frostig, Yeoshua |
description | The linear elasticity problem formulation and solution for a generally asymmetric sandwich curved beam/panel consisting of orthotropic core and face sheets, which is subjected to a top face sinusoidal distributed transverse loading, is presented. The displacement approach is used along with a plane strain assumption, and the panel is assumed to be simply supported at the ends. Closed-form solutions for the displacements and stresses are derived, and results for realistic material systems are presented for the transverse and hoop displacements as well as the core transverse normal and shear stresses and the face hoop stresses. A comparison of the results between the elasticity, the first-order shear deformation theory with an equivalent shear modulus, and the classical sandwich theories is presented. In addition, a comparison is presented with results from the compressive high-order sandwich panel theory. This closed-form elasticity solution can be used as a benchmark in assessing the accuracy of the various sandwich panel theories or numerical approaches. |
doi_str_mv | 10.2514/1.J055760 |
format | article |
fullrecord | <record><control><sourceid>proquest_cross</sourceid><recordid>TN_cdi_crossref_primary_10_2514_1_J055760</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>2167391067</sourcerecordid><originalsourceid>FETCH-LOGICAL-a351t-c456d1a6fe4eb320f8e22d5572293dacd9df69b92199afc6ddb5d2323045b0b73</originalsourceid><addsrcrecordid>eNp9kF1LwzAUhoMoOKcX_oOAIHjRLSdp0uZSx_xCUNgEL4SSNinL6JqZpI79ezs28ELw6vAeHp7DeRG6BDKiHNIxjJ4J55kgR2gAnLGE5fzjGA0IIZBAyukpOgth2Sea5TBAn9NGhWgrG7d45pouWtfi2nk86fy30XimWr2x1QLfGbUK4zfVmibgfoknbrVW3oae39i4wLPouyp2XjV4vjDOWxPO0UmtmmAuDnOI3u-n88lj8vL68DS5fUkU4xCTKuVCgxK1SU3JKKlzQ6nuv6BUMq0qLXUtZCkpSKnqSmhdck0ZZSTlJSkzNkRXe-_au6_OhFgsXefb_mRBUwmC5pzm_1IgMiaBiJ3rZk9V3oXgTV2svV0pvy2AFLuKCygOFffs9Z5VVqlf21_wB6FaeUU</addsrcrecordid><sourcetype>Aggregation Database</sourcetype><iscdi>true</iscdi><recordtype>article</recordtype><pqid>2167391067</pqid></control><display><type>article</type><title>Elasticity Solution for Curved Sandwich Beams/Panels and Comparison with Structural Theories</title><source>Alma/SFX Local Collection</source><creator>Kardomateas, George A ; Rodcheuy, Nunthadech ; Frostig, Yeoshua</creator><creatorcontrib>Kardomateas, George A ; Rodcheuy, Nunthadech ; Frostig, Yeoshua</creatorcontrib><description>The linear elasticity problem formulation and solution for a generally asymmetric sandwich curved beam/panel consisting of orthotropic core and face sheets, which is subjected to a top face sinusoidal distributed transverse loading, is presented. The displacement approach is used along with a plane strain assumption, and the panel is assumed to be simply supported at the ends. Closed-form solutions for the displacements and stresses are derived, and results for realistic material systems are presented for the transverse and hoop displacements as well as the core transverse normal and shear stresses and the face hoop stresses. A comparison of the results between the elasticity, the first-order shear deformation theory with an equivalent shear modulus, and the classical sandwich theories is presented. In addition, a comparison is presented with results from the compressive high-order sandwich panel theory. This closed-form elasticity solution can be used as a benchmark in assessing the accuracy of the various sandwich panel theories or numerical approaches.</description><identifier>ISSN: 0001-1452</identifier><identifier>EISSN: 1533-385X</identifier><identifier>DOI: 10.2514/1.J055760</identifier><language>eng</language><publisher>Virginia: American Institute of Aeronautics and Astronautics</publisher><subject>Beams (structural) ; Closed form solutions ; Curved beams ; Curved panels ; Deformation ; Displacement ; Elasticity ; Exact solutions ; Hoops ; Load distribution (forces) ; Plane strain ; Sandwich panels ; Sandwich structures ; Shear deformation ; Shear modulus ; Shear stress ; Stress concentration ; Transverse loads</subject><ispartof>AIAA journal, 2017-09, Vol.55 (9), p.3153-3160</ispartof><rights>Copyright © 2017 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 ; employ the ISSN (print) or (online) to initiate your request. See also AIAA Rights and Permissions .</rights><rights>Copyright © 2017 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 ISSN 0001-1452 (print) or 1533-385X (online) to initiate your request. See also AIAA Rights and Permissions www.aiaa.org/randp.</rights><lds50>peer_reviewed</lds50><oa>free_for_read</oa><woscitedreferencessubscribed>false</woscitedreferencessubscribed><citedby>FETCH-LOGICAL-a351t-c456d1a6fe4eb320f8e22d5572293dacd9df69b92199afc6ddb5d2323045b0b73</citedby><cites>FETCH-LOGICAL-a351t-c456d1a6fe4eb320f8e22d5572293dacd9df69b92199afc6ddb5d2323045b0b73</cites></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><link.rule.ids>314,780,784,27923,27924</link.rule.ids></links><search><creatorcontrib>Kardomateas, George A</creatorcontrib><creatorcontrib>Rodcheuy, Nunthadech</creatorcontrib><creatorcontrib>Frostig, Yeoshua</creatorcontrib><title>Elasticity Solution for Curved Sandwich Beams/Panels and Comparison with Structural Theories</title><title>AIAA journal</title><description>The linear elasticity problem formulation and solution for a generally asymmetric sandwich curved beam/panel consisting of orthotropic core and face sheets, which is subjected to a top face sinusoidal distributed transverse loading, is presented. The displacement approach is used along with a plane strain assumption, and the panel is assumed to be simply supported at the ends. Closed-form solutions for the displacements and stresses are derived, and results for realistic material systems are presented for the transverse and hoop displacements as well as the core transverse normal and shear stresses and the face hoop stresses. A comparison of the results between the elasticity, the first-order shear deformation theory with an equivalent shear modulus, and the classical sandwich theories is presented. In addition, a comparison is presented with results from the compressive high-order sandwich panel theory. This closed-form elasticity solution can be used as a benchmark in assessing the accuracy of the various sandwich panel theories or numerical approaches.</description><subject>Beams (structural)</subject><subject>Closed form solutions</subject><subject>Curved beams</subject><subject>Curved panels</subject><subject>Deformation</subject><subject>Displacement</subject><subject>Elasticity</subject><subject>Exact solutions</subject><subject>Hoops</subject><subject>Load distribution (forces)</subject><subject>Plane strain</subject><subject>Sandwich panels</subject><subject>Sandwich structures</subject><subject>Shear deformation</subject><subject>Shear modulus</subject><subject>Shear stress</subject><subject>Stress concentration</subject><subject>Transverse loads</subject><issn>0001-1452</issn><issn>1533-385X</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2017</creationdate><recordtype>article</recordtype><recordid>eNp9kF1LwzAUhoMoOKcX_oOAIHjRLSdp0uZSx_xCUNgEL4SSNinL6JqZpI79ezs28ELw6vAeHp7DeRG6BDKiHNIxjJ4J55kgR2gAnLGE5fzjGA0IIZBAyukpOgth2Sea5TBAn9NGhWgrG7d45pouWtfi2nk86fy30XimWr2x1QLfGbUK4zfVmibgfoknbrVW3oae39i4wLPouyp2XjV4vjDOWxPO0UmtmmAuDnOI3u-n88lj8vL68DS5fUkU4xCTKuVCgxK1SU3JKKlzQ6nuv6BUMq0qLXUtZCkpSKnqSmhdck0ZZSTlJSkzNkRXe-_au6_OhFgsXefb_mRBUwmC5pzm_1IgMiaBiJ3rZk9V3oXgTV2svV0pvy2AFLuKCygOFffs9Z5VVqlf21_wB6FaeUU</recordid><startdate>20170901</startdate><enddate>20170901</enddate><creator>Kardomateas, George A</creator><creator>Rodcheuy, Nunthadech</creator><creator>Frostig, Yeoshua</creator><general>American Institute of Aeronautics and Astronautics</general><scope>AAYXX</scope><scope>CITATION</scope><scope>7TB</scope><scope>8FD</scope><scope>FR3</scope><scope>H8D</scope><scope>L7M</scope></search><sort><creationdate>20170901</creationdate><title>Elasticity Solution for Curved Sandwich Beams/Panels and Comparison with Structural Theories</title><author>Kardomateas, George A ; Rodcheuy, Nunthadech ; Frostig, Yeoshua</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-a351t-c456d1a6fe4eb320f8e22d5572293dacd9df69b92199afc6ddb5d2323045b0b73</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2017</creationdate><topic>Beams (structural)</topic><topic>Closed form solutions</topic><topic>Curved beams</topic><topic>Curved panels</topic><topic>Deformation</topic><topic>Displacement</topic><topic>Elasticity</topic><topic>Exact solutions</topic><topic>Hoops</topic><topic>Load distribution (forces)</topic><topic>Plane strain</topic><topic>Sandwich panels</topic><topic>Sandwich structures</topic><topic>Shear deformation</topic><topic>Shear modulus</topic><topic>Shear stress</topic><topic>Stress concentration</topic><topic>Transverse loads</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Kardomateas, George A</creatorcontrib><creatorcontrib>Rodcheuy, Nunthadech</creatorcontrib><creatorcontrib>Frostig, Yeoshua</creatorcontrib><collection>CrossRef</collection><collection>Mechanical & Transportation Engineering Abstracts</collection><collection>Technology Research Database</collection><collection>Engineering Research Database</collection><collection>Aerospace Database</collection><collection>Advanced Technologies Database with Aerospace</collection><jtitle>AIAA journal</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Kardomateas, George A</au><au>Rodcheuy, Nunthadech</au><au>Frostig, Yeoshua</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Elasticity Solution for Curved Sandwich Beams/Panels and Comparison with Structural Theories</atitle><jtitle>AIAA journal</jtitle><date>2017-09-01</date><risdate>2017</risdate><volume>55</volume><issue>9</issue><spage>3153</spage><epage>3160</epage><pages>3153-3160</pages><issn>0001-1452</issn><eissn>1533-385X</eissn><abstract>The linear elasticity problem formulation and solution for a generally asymmetric sandwich curved beam/panel consisting of orthotropic core and face sheets, which is subjected to a top face sinusoidal distributed transverse loading, is presented. The displacement approach is used along with a plane strain assumption, and the panel is assumed to be simply supported at the ends. Closed-form solutions for the displacements and stresses are derived, and results for realistic material systems are presented for the transverse and hoop displacements as well as the core transverse normal and shear stresses and the face hoop stresses. A comparison of the results between the elasticity, the first-order shear deformation theory with an equivalent shear modulus, and the classical sandwich theories is presented. In addition, a comparison is presented with results from the compressive high-order sandwich panel theory. This closed-form elasticity solution can be used as a benchmark in assessing the accuracy of the various sandwich panel theories or numerical approaches.</abstract><cop>Virginia</cop><pub>American Institute of Aeronautics and Astronautics</pub><doi>10.2514/1.J055760</doi><tpages>8</tpages><oa>free_for_read</oa></addata></record> |
fulltext | fulltext |
identifier | ISSN: 0001-1452 |
ispartof | AIAA journal, 2017-09, Vol.55 (9), p.3153-3160 |
issn | 0001-1452 1533-385X |
language | eng |
recordid | cdi_crossref_primary_10_2514_1_J055760 |
source | Alma/SFX Local Collection |
subjects | Beams (structural) Closed form solutions Curved beams Curved panels Deformation Displacement Elasticity Exact solutions Hoops Load distribution (forces) Plane strain Sandwich panels Sandwich structures Shear deformation Shear modulus Shear stress Stress concentration Transverse loads |
title | Elasticity Solution for Curved Sandwich Beams/Panels and Comparison with Structural Theories |
url | http://sfxeu10.hosted.exlibrisgroup.com/loughborough?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-01-11T15%3A25%3A31IST&url_ver=Z39.88-2004&url_ctx_fmt=infofi/fmt:kev:mtx:ctx&rfr_id=info:sid/primo.exlibrisgroup.com:primo3-Article-proquest_cross&rft_val_fmt=info:ofi/fmt:kev:mtx:journal&rft.genre=article&rft.atitle=Elasticity%20Solution%20for%20Curved%20Sandwich%20Beams/Panels%20and%20Comparison%20with%20Structural%20Theories&rft.jtitle=AIAA%20journal&rft.au=Kardomateas,%20George%20A&rft.date=2017-09-01&rft.volume=55&rft.issue=9&rft.spage=3153&rft.epage=3160&rft.pages=3153-3160&rft.issn=0001-1452&rft.eissn=1533-385X&rft_id=info:doi/10.2514/1.J055760&rft_dat=%3Cproquest_cross%3E2167391067%3C/proquest_cross%3E%3Cgrp_id%3Ecdi_FETCH-LOGICAL-a351t-c456d1a6fe4eb320f8e22d5572293dacd9df69b92199afc6ddb5d2323045b0b73%3C/grp_id%3E%3Coa%3E%3C/oa%3E%3Curl%3E%3C/url%3E&rft_id=info:oai/&rft_pqid=2167391067&rft_id=info:pmid/&rfr_iscdi=true |