Interaction formulae for buckling and failure of orthotropic plates under combined axial compression/tension and shear
An interaction function was constructed based on the axial compression/tension and shear loads of orthotropic plates. The coefficients of the polynomial function were determined by uniaxial test results. Buckling interaction and failure interaction formulae under combined axial tension/compression a...
Gespeichert in:
Veröffentlicht in: | Chinese journal of aeronautics 2022-03, Vol.35 (3), p.272-280 |
---|---|
Hauptverfasser: | , , , , , |
Format: | Artikel |
Sprache: | eng |
Schlagworte: | |
Online-Zugang: | Volltext |
Tags: |
Tag hinzufügen
Keine Tags, Fügen Sie den ersten Tag hinzu!
|
container_end_page | 280 |
---|---|
container_issue | 3 |
container_start_page | 272 |
container_title | Chinese journal of aeronautics |
container_volume | 35 |
creator | WANG, Binwen CHEN, Xiangming SUN, Xiasheng CHEN, Puhui WANG, Zhe CHAI, Ya'nan |
description | An interaction function was constructed based on the axial compression/tension and shear loads of orthotropic plates. The coefficients of the polynomial function were determined by uniaxial test results. Buckling interaction and failure interaction formulae under combined axial tension/compression and shear loads were established. Based on the uniaxial load test results of orthotropic plates, the buckling load and bearing capacity under any proportion of the combined loads could be predicted by using the proposed interaction formulae. The buckling interaction curves and failure envelopes predicted by the proposed interaction formulae were in excellent agreement with the test results. |
doi_str_mv | 10.1016/j.cja.2021.01.021 |
format | Article |
fullrecord | <record><control><sourceid>wanfang_jour_cross</sourceid><recordid>TN_cdi_wanfang_journals_hkxb_e202203020</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><wanfj_id>hkxb_e202203020</wanfj_id><els_id>S1000936121000674</els_id><sourcerecordid>hkxb_e202203020</sourcerecordid><originalsourceid>FETCH-LOGICAL-c372t-90866a5979cfdc72b1e7c86c133a5e88b832e288e626e125efc0f3f938206f683</originalsourceid><addsrcrecordid>eNp9UE1LAzEQzUHBWv0B3nLz1DpJaDaLJyl-QcGLnkM2O7FZt0lJdqv-e7PWs_CGNwPz3jCPkCsGSwZM3nRL25klB86WUMDZCZkxAFjUQrIzcp5zByDqisGMHJ7DgMnYwcdAXUy7sTc4NbQZ7Ufvwzs1oaXO-H5MSKOjMQ3bOKS495buezNgpmNoMVEbd40P2FLz5U0_jfuEORfjmwHDxL9WeYsmXZBTZ_qMl388J28P96_rp8Xm5fF5fbdZWFHxYVGDktKs6qq2rrUVbxhWVknLhDArVKpRgiNXCiWXyPgKnQUnXC0UB-mkEnNyffT9NMGZ8K67OKZQLurtx1ejsYTEQUCpOWHHTZtizgmd3ie_M-lbM9BTrLrTJVY9xaqhgLOiuT1qsLxw8Jh0th6DxdYntINuo_9H_QNn14Pq</addsrcrecordid><sourcetype>Aggregation Database</sourcetype><iscdi>true</iscdi><recordtype>article</recordtype></control><display><type>article</type><title>Interaction formulae for buckling and failure of orthotropic plates under combined axial compression/tension and shear</title><source>Elsevier ScienceDirect Journals</source><source>Elektronische Zeitschriftenbibliothek - Frei zugängliche E-Journals</source><creator>WANG, Binwen ; CHEN, Xiangming ; SUN, Xiasheng ; CHEN, Puhui ; WANG, Zhe ; CHAI, Ya'nan</creator><creatorcontrib>WANG, Binwen ; CHEN, Xiangming ; SUN, Xiasheng ; CHEN, Puhui ; WANG, Zhe ; CHAI, Ya'nan</creatorcontrib><description>An interaction function was constructed based on the axial compression/tension and shear loads of orthotropic plates. The coefficients of the polynomial function were determined by uniaxial test results. Buckling interaction and failure interaction formulae under combined axial tension/compression and shear loads were established. Based on the uniaxial load test results of orthotropic plates, the buckling load and bearing capacity under any proportion of the combined loads could be predicted by using the proposed interaction formulae. The buckling interaction curves and failure envelopes predicted by the proposed interaction formulae were in excellent agreement with the test results.</description><identifier>ISSN: 1000-9361</identifier><identifier>DOI: 10.1016/j.cja.2021.01.021</identifier><language>eng</language><publisher>Elsevier Ltd</publisher><subject>Buckling ; Combined loads ; Failure ; Interaction formulae ; Orthotropic plate</subject><ispartof>Chinese journal of aeronautics, 2022-03, Vol.35 (3), p.272-280</ispartof><rights>2021 Chinese Society of Aeronautics and Astronautics</rights><rights>Copyright © Wanfang Data Co. Ltd. All Rights Reserved.</rights><lds50>peer_reviewed</lds50><oa>free_for_read</oa><woscitedreferencessubscribed>false</woscitedreferencessubscribed><citedby>FETCH-LOGICAL-c372t-90866a5979cfdc72b1e7c86c133a5e88b832e288e626e125efc0f3f938206f683</citedby><cites>FETCH-LOGICAL-c372t-90866a5979cfdc72b1e7c86c133a5e88b832e288e626e125efc0f3f938206f683</cites><orcidid>0000-0002-2571-3539</orcidid></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Uhttp://www.wanfangdata.com.cn/images/PeriodicalImages/hkxb-e/hkxb-e.jpg</thumbnail><linktohtml>$$Uhttps://dx.doi.org/10.1016/j.cja.2021.01.021$$EHTML$$P50$$Gelsevier$$Hfree_for_read</linktohtml><link.rule.ids>314,777,781,3537,27905,27906,45976</link.rule.ids></links><search><creatorcontrib>WANG, Binwen</creatorcontrib><creatorcontrib>CHEN, Xiangming</creatorcontrib><creatorcontrib>SUN, Xiasheng</creatorcontrib><creatorcontrib>CHEN, Puhui</creatorcontrib><creatorcontrib>WANG, Zhe</creatorcontrib><creatorcontrib>CHAI, Ya'nan</creatorcontrib><title>Interaction formulae for buckling and failure of orthotropic plates under combined axial compression/tension and shear</title><title>Chinese journal of aeronautics</title><description>An interaction function was constructed based on the axial compression/tension and shear loads of orthotropic plates. The coefficients of the polynomial function were determined by uniaxial test results. Buckling interaction and failure interaction formulae under combined axial tension/compression and shear loads were established. Based on the uniaxial load test results of orthotropic plates, the buckling load and bearing capacity under any proportion of the combined loads could be predicted by using the proposed interaction formulae. The buckling interaction curves and failure envelopes predicted by the proposed interaction formulae were in excellent agreement with the test results.</description><subject>Buckling</subject><subject>Combined loads</subject><subject>Failure</subject><subject>Interaction formulae</subject><subject>Orthotropic plate</subject><issn>1000-9361</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2022</creationdate><recordtype>article</recordtype><recordid>eNp9UE1LAzEQzUHBWv0B3nLz1DpJaDaLJyl-QcGLnkM2O7FZt0lJdqv-e7PWs_CGNwPz3jCPkCsGSwZM3nRL25klB86WUMDZCZkxAFjUQrIzcp5zByDqisGMHJ7DgMnYwcdAXUy7sTc4NbQZ7Ufvwzs1oaXO-H5MSKOjMQ3bOKS495buezNgpmNoMVEbd40P2FLz5U0_jfuEORfjmwHDxL9WeYsmXZBTZ_qMl388J28P96_rp8Xm5fF5fbdZWFHxYVGDktKs6qq2rrUVbxhWVknLhDArVKpRgiNXCiWXyPgKnQUnXC0UB-mkEnNyffT9NMGZ8K67OKZQLurtx1ejsYTEQUCpOWHHTZtizgmd3ie_M-lbM9BTrLrTJVY9xaqhgLOiuT1qsLxw8Jh0th6DxdYntINuo_9H_QNn14Pq</recordid><startdate>20220301</startdate><enddate>20220301</enddate><creator>WANG, Binwen</creator><creator>CHEN, Xiangming</creator><creator>SUN, Xiasheng</creator><creator>CHEN, Puhui</creator><creator>WANG, Zhe</creator><creator>CHAI, Ya'nan</creator><general>Elsevier Ltd</general><general>Aeronautics Science and Technology Key Laboratory of Full Scale Aircraft Structure and Fatigue,Aircraft Strength Research Institute of China,Xi'an 710065,China%Chinese Aeronautical Establishment,Beijing 100029,China%State Key Laboratory of Mechanics and Control of Mechanical Structures,Nanjing University of Aeronautics and Astronautics,Nanjing 210016,China</general><scope>6I.</scope><scope>AAFTH</scope><scope>AAYXX</scope><scope>CITATION</scope><scope>2B.</scope><scope>4A8</scope><scope>92I</scope><scope>93N</scope><scope>PSX</scope><scope>TCJ</scope><orcidid>https://orcid.org/0000-0002-2571-3539</orcidid></search><sort><creationdate>20220301</creationdate><title>Interaction formulae for buckling and failure of orthotropic plates under combined axial compression/tension and shear</title><author>WANG, Binwen ; CHEN, Xiangming ; SUN, Xiasheng ; CHEN, Puhui ; WANG, Zhe ; CHAI, Ya'nan</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-c372t-90866a5979cfdc72b1e7c86c133a5e88b832e288e626e125efc0f3f938206f683</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2022</creationdate><topic>Buckling</topic><topic>Combined loads</topic><topic>Failure</topic><topic>Interaction formulae</topic><topic>Orthotropic plate</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>WANG, Binwen</creatorcontrib><creatorcontrib>CHEN, Xiangming</creatorcontrib><creatorcontrib>SUN, Xiasheng</creatorcontrib><creatorcontrib>CHEN, Puhui</creatorcontrib><creatorcontrib>WANG, Zhe</creatorcontrib><creatorcontrib>CHAI, Ya'nan</creatorcontrib><collection>ScienceDirect Open Access Titles</collection><collection>Elsevier:ScienceDirect:Open Access</collection><collection>CrossRef</collection><collection>Wanfang Data Journals - Hong Kong</collection><collection>WANFANG Data Centre</collection><collection>Wanfang Data Journals</collection><collection>万方数据期刊 - 香港版</collection><collection>China Online Journals (COJ)</collection><collection>China Online Journals (COJ)</collection><jtitle>Chinese journal of aeronautics</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>WANG, Binwen</au><au>CHEN, Xiangming</au><au>SUN, Xiasheng</au><au>CHEN, Puhui</au><au>WANG, Zhe</au><au>CHAI, Ya'nan</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Interaction formulae for buckling and failure of orthotropic plates under combined axial compression/tension and shear</atitle><jtitle>Chinese journal of aeronautics</jtitle><date>2022-03-01</date><risdate>2022</risdate><volume>35</volume><issue>3</issue><spage>272</spage><epage>280</epage><pages>272-280</pages><issn>1000-9361</issn><abstract>An interaction function was constructed based on the axial compression/tension and shear loads of orthotropic plates. The coefficients of the polynomial function were determined by uniaxial test results. Buckling interaction and failure interaction formulae under combined axial tension/compression and shear loads were established. Based on the uniaxial load test results of orthotropic plates, the buckling load and bearing capacity under any proportion of the combined loads could be predicted by using the proposed interaction formulae. The buckling interaction curves and failure envelopes predicted by the proposed interaction formulae were in excellent agreement with the test results.</abstract><pub>Elsevier Ltd</pub><doi>10.1016/j.cja.2021.01.021</doi><tpages>9</tpages><orcidid>https://orcid.org/0000-0002-2571-3539</orcidid><oa>free_for_read</oa></addata></record> |
fulltext | fulltext |
identifier | ISSN: 1000-9361 |
ispartof | Chinese journal of aeronautics, 2022-03, Vol.35 (3), p.272-280 |
issn | 1000-9361 |
language | eng |
recordid | cdi_wanfang_journals_hkxb_e202203020 |
source | Elsevier ScienceDirect Journals; Elektronische Zeitschriftenbibliothek - Frei zugängliche E-Journals |
subjects | Buckling Combined loads Failure Interaction formulae Orthotropic plate |
title | Interaction formulae for buckling and failure of orthotropic plates under combined axial compression/tension and shear |
url | https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-01-19T01%3A08%3A53IST&url_ver=Z39.88-2004&url_ctx_fmt=infofi/fmt:kev:mtx:ctx&rfr_id=info:sid/primo.exlibrisgroup.com:primo3-Article-wanfang_jour_cross&rft_val_fmt=info:ofi/fmt:kev:mtx:journal&rft.genre=article&rft.atitle=Interaction%20formulae%20for%20buckling%20and%20failure%20of%20orthotropic%20plates%20under%20combined%20axial%20compression/tension%20and%20shear&rft.jtitle=Chinese%20journal%20of%20aeronautics&rft.au=WANG,%20Binwen&rft.date=2022-03-01&rft.volume=35&rft.issue=3&rft.spage=272&rft.epage=280&rft.pages=272-280&rft.issn=1000-9361&rft_id=info:doi/10.1016/j.cja.2021.01.021&rft_dat=%3Cwanfang_jour_cross%3Ehkxb_e202203020%3C/wanfang_jour_cross%3E%3Curl%3E%3C/url%3E&disable_directlink=true&sfx.directlink=off&sfx.report_link=0&rft_id=info:oai/&rft_id=info:pmid/&rft_wanfj_id=hkxb_e202203020&rft_els_id=S1000936121000674&rfr_iscdi=true |