An Elastic-Plastic Stress Analysis of Symmetric Aluminum Metal-Matrix Composite Laminated Plates under Thermal Loads
In this study, a thermal elastic-plastic stress analysis is carried out on symmetric cross-ply (0°/90°)2 and angle-ply (30°/30°)2, (45°/45°)2, (60°/60°)2 aluminum metal-matrix composite laminated plates. Temperature changes parabolically from T0 up to T0 along the thickness. It is zero on the middle...
Gespeichert in:
| Veröffentlicht in: | Journal of reinforced plastics and composites 2004-08, Vol.23 (12), p.1301-1312 |
|---|---|
| Hauptverfasser: | , |
| Format: | Artikel |
| Sprache: | eng |
| Schlagworte: | |
| Online-Zugang: | Volltext |
| Tags: |
Tag hinzufügen
Keine Tags, Fügen Sie den ersten Tag hinzu!
|
| container_end_page | 1312 |
|---|---|
| container_issue | 12 |
| container_start_page | 1301 |
| container_title | Journal of reinforced plastics and composites |
| container_volume | 23 |
| creator | Topcu, Muzaffer Ondurucu, Ayse |
| description | In this study, a thermal elastic-plastic stress analysis is carried out on symmetric cross-ply (0°/90°)2 and angle-ply (30°/30°)2, (45°/45°)2, (60°/60°)2 aluminum metal-matrix composite laminated plates. Temperature changes parabolically from T0 up to T0 along the thickness. It is zero on the middle axis. The composite material is assumed to be linear strain hardening. The Tsai-Hill Theory is used as a yield criterion. The elastic-plastic solution is carried out for small plastic deformations. The distributions residual stress components of σ
x
and σ
y
are illustrated along the thickness of the laminated plates. All the residual stress moments are in static balance with respect to middle plane of the laminates since they are symmetric in opposite signs. |
| doi_str_mv | 10.1177/0731684404037047 |
| format | Article |
| fullrecord | <record><control><sourceid>proquest_cross</sourceid><recordid>TN_cdi_proquest_miscellaneous_28623466</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sage_id>10.1177_0731684404037047</sage_id><sourcerecordid>28255216</sourcerecordid><originalsourceid>FETCH-LOGICAL-c402t-93143e72e682ff8aa3ca92a0b004b9d558946cd43c590570885dcc49e634c2603</originalsourceid><addsrcrecordid>eNqNkc9rFEEQhRtRcI3ePfZFb2Oqf88clyVGYYNC4nmo9NTohJ6ZtasH3P_eWTYgBIScCup977s8Id4r-KRUCJcQjPK1tWDBBLDhhdgoZ6AKjbcvxeYUV6f8tXjD_ACglbV2I8p2klcJuQyx-n6-8rZkYpbbCdORB5ZzL2-P40glr-E2LeMwLaO8oYKpusH1-0fu5vEw81BI7nGNsVAnV10hlsvUUZZ3vyiPmOR-xo7filc9JqZ3j_dC_Ph8dbf7Uu2_XX_dbfdVtKBL1RhlDQVNvtZ9XyOaiI1GuAew903nXN1YHztromvABahr18VoG_LGRu3BXIiPZ-8hz78X4tKOA0dKCSeaF2517bWx3j8D1EH7JjwHdE6rkxHOYMwzc6a-PeRhxHxsFbSnwdqng62VD49u5IipzzjFgf_1PEBtnVm56swx_qT2YV7yOhT_3_sXbxehlw</addsrcrecordid><sourcetype>Aggregation Database</sourcetype><iscdi>true</iscdi><recordtype>article</recordtype><pqid>28255216</pqid></control><display><type>article</type><title>An Elastic-Plastic Stress Analysis of Symmetric Aluminum Metal-Matrix Composite Laminated Plates under Thermal Loads</title><source>SAGE Complete A-Z List</source><creator>Topcu, Muzaffer ; Ondurucu, Ayse</creator><creatorcontrib>Topcu, Muzaffer ; Ondurucu, Ayse</creatorcontrib><description>In this study, a thermal elastic-plastic stress analysis is carried out on symmetric cross-ply (0°/90°)2 and angle-ply (30°/30°)2, (45°/45°)2, (60°/60°)2 aluminum metal-matrix composite laminated plates. Temperature changes parabolically from T0 up to T0 along the thickness. It is zero on the middle axis. The composite material is assumed to be linear strain hardening. The Tsai-Hill Theory is used as a yield criterion. The elastic-plastic solution is carried out for small plastic deformations. The distributions residual stress components of σ
x
and σ
y
are illustrated along the thickness of the laminated plates. All the residual stress moments are in static balance with respect to middle plane of the laminates since they are symmetric in opposite signs.</description><identifier>ISSN: 0731-6844</identifier><identifier>EISSN: 1530-7964</identifier><identifier>DOI: 10.1177/0731684404037047</identifier><identifier>CODEN: JRPCDW</identifier><language>eng</language><publisher>Thousand Oaks, CA: SAGE Publications</publisher><subject>Applied sciences ; Composites ; Exact sciences and technology ; Forms of application and semi-finished materials ; Laminates ; Polymer industry, paints, wood ; Technology of polymers</subject><ispartof>Journal of reinforced plastics and composites, 2004-08, Vol.23 (12), p.1301-1312</ispartof><rights>2005 INIST-CNRS</rights><lds50>peer_reviewed</lds50><woscitedreferencessubscribed>false</woscitedreferencessubscribed><citedby>FETCH-LOGICAL-c402t-93143e72e682ff8aa3ca92a0b004b9d558946cd43c590570885dcc49e634c2603</citedby><cites>FETCH-LOGICAL-c402t-93143e72e682ff8aa3ca92a0b004b9d558946cd43c590570885dcc49e634c2603</cites></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><linktopdf>$$Uhttps://journals.sagepub.com/doi/pdf/10.1177/0731684404037047$$EPDF$$P50$$Gsage$$H</linktopdf><linktohtml>$$Uhttps://journals.sagepub.com/doi/10.1177/0731684404037047$$EHTML$$P50$$Gsage$$H</linktohtml><link.rule.ids>314,776,780,21798,27901,27902,43597,43598</link.rule.ids><backlink>$$Uhttp://pascal-francis.inist.fr/vibad/index.php?action=getRecordDetail&idt=16008453$$DView record in Pascal Francis$$Hfree_for_read</backlink></links><search><creatorcontrib>Topcu, Muzaffer</creatorcontrib><creatorcontrib>Ondurucu, Ayse</creatorcontrib><title>An Elastic-Plastic Stress Analysis of Symmetric Aluminum Metal-Matrix Composite Laminated Plates under Thermal Loads</title><title>Journal of reinforced plastics and composites</title><description>In this study, a thermal elastic-plastic stress analysis is carried out on symmetric cross-ply (0°/90°)2 and angle-ply (30°/30°)2, (45°/45°)2, (60°/60°)2 aluminum metal-matrix composite laminated plates. Temperature changes parabolically from T0 up to T0 along the thickness. It is zero on the middle axis. The composite material is assumed to be linear strain hardening. The Tsai-Hill Theory is used as a yield criterion. The elastic-plastic solution is carried out for small plastic deformations. The distributions residual stress components of σ
x
and σ
y
are illustrated along the thickness of the laminated plates. All the residual stress moments are in static balance with respect to middle plane of the laminates since they are symmetric in opposite signs.</description><subject>Applied sciences</subject><subject>Composites</subject><subject>Exact sciences and technology</subject><subject>Forms of application and semi-finished materials</subject><subject>Laminates</subject><subject>Polymer industry, paints, wood</subject><subject>Technology of polymers</subject><issn>0731-6844</issn><issn>1530-7964</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2004</creationdate><recordtype>article</recordtype><recordid>eNqNkc9rFEEQhRtRcI3ePfZFb2Oqf88clyVGYYNC4nmo9NTohJ6ZtasH3P_eWTYgBIScCup977s8Id4r-KRUCJcQjPK1tWDBBLDhhdgoZ6AKjbcvxeYUV6f8tXjD_ACglbV2I8p2klcJuQyx-n6-8rZkYpbbCdORB5ZzL2-P40glr-E2LeMwLaO8oYKpusH1-0fu5vEw81BI7nGNsVAnV10hlsvUUZZ3vyiPmOR-xo7filc9JqZ3j_dC_Ph8dbf7Uu2_XX_dbfdVtKBL1RhlDQVNvtZ9XyOaiI1GuAew903nXN1YHztromvABahr18VoG_LGRu3BXIiPZ-8hz78X4tKOA0dKCSeaF2517bWx3j8D1EH7JjwHdE6rkxHOYMwzc6a-PeRhxHxsFbSnwdqng62VD49u5IipzzjFgf_1PEBtnVm56swx_qT2YV7yOhT_3_sXbxehlw</recordid><startdate>200408</startdate><enddate>200408</enddate><creator>Topcu, Muzaffer</creator><creator>Ondurucu, Ayse</creator><general>SAGE Publications</general><general>Sage</general><scope>IQODW</scope><scope>AAYXX</scope><scope>CITATION</scope><scope>7QF</scope><scope>8BQ</scope><scope>8FD</scope><scope>H8D</scope><scope>JG9</scope><scope>L7M</scope><scope>7TB</scope><scope>FR3</scope></search><sort><creationdate>200408</creationdate><title>An Elastic-Plastic Stress Analysis of Symmetric Aluminum Metal-Matrix Composite Laminated Plates under Thermal Loads</title><author>Topcu, Muzaffer ; Ondurucu, Ayse</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-c402t-93143e72e682ff8aa3ca92a0b004b9d558946cd43c590570885dcc49e634c2603</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2004</creationdate><topic>Applied sciences</topic><topic>Composites</topic><topic>Exact sciences and technology</topic><topic>Forms of application and semi-finished materials</topic><topic>Laminates</topic><topic>Polymer industry, paints, wood</topic><topic>Technology of polymers</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Topcu, Muzaffer</creatorcontrib><creatorcontrib>Ondurucu, Ayse</creatorcontrib><collection>Pascal-Francis</collection><collection>CrossRef</collection><collection>Aluminium Industry Abstracts</collection><collection>METADEX</collection><collection>Technology Research Database</collection><collection>Aerospace Database</collection><collection>Materials Research Database</collection><collection>Advanced Technologies Database with Aerospace</collection><collection>Mechanical & Transportation Engineering Abstracts</collection><collection>Engineering Research Database</collection><jtitle>Journal of reinforced plastics and composites</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Topcu, Muzaffer</au><au>Ondurucu, Ayse</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>An Elastic-Plastic Stress Analysis of Symmetric Aluminum Metal-Matrix Composite Laminated Plates under Thermal Loads</atitle><jtitle>Journal of reinforced plastics and composites</jtitle><date>2004-08</date><risdate>2004</risdate><volume>23</volume><issue>12</issue><spage>1301</spage><epage>1312</epage><pages>1301-1312</pages><issn>0731-6844</issn><eissn>1530-7964</eissn><coden>JRPCDW</coden><abstract>In this study, a thermal elastic-plastic stress analysis is carried out on symmetric cross-ply (0°/90°)2 and angle-ply (30°/30°)2, (45°/45°)2, (60°/60°)2 aluminum metal-matrix composite laminated plates. Temperature changes parabolically from T0 up to T0 along the thickness. It is zero on the middle axis. The composite material is assumed to be linear strain hardening. The Tsai-Hill Theory is used as a yield criterion. The elastic-plastic solution is carried out for small plastic deformations. The distributions residual stress components of σ
x
and σ
y
are illustrated along the thickness of the laminated plates. All the residual stress moments are in static balance with respect to middle plane of the laminates since they are symmetric in opposite signs.</abstract><cop>Thousand Oaks, CA</cop><pub>SAGE Publications</pub><doi>10.1177/0731684404037047</doi><tpages>12</tpages></addata></record> |
| fulltext | fulltext |
| identifier | ISSN: 0731-6844 |
| ispartof | Journal of reinforced plastics and composites, 2004-08, Vol.23 (12), p.1301-1312 |
| issn | 0731-6844 1530-7964 |
| language | eng |
| recordid | cdi_proquest_miscellaneous_28623466 |
| source | SAGE Complete A-Z List |
| subjects | Applied sciences Composites Exact sciences and technology Forms of application and semi-finished materials Laminates Polymer industry, paints, wood Technology of polymers |
| title | An Elastic-Plastic Stress Analysis of Symmetric Aluminum Metal-Matrix Composite Laminated Plates under Thermal Loads |
| url | https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-02-06T18%3A31%3A06IST&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=An%20Elastic-Plastic%20Stress%20Analysis%20of%20Symmetric%20Aluminum%20Metal-Matrix%20Composite%20Laminated%20Plates%20under%20Thermal%20Loads&rft.jtitle=Journal%20of%20reinforced%20plastics%20and%20composites&rft.au=Topcu,%20Muzaffer&rft.date=2004-08&rft.volume=23&rft.issue=12&rft.spage=1301&rft.epage=1312&rft.pages=1301-1312&rft.issn=0731-6844&rft.eissn=1530-7964&rft.coden=JRPCDW&rft_id=info:doi/10.1177/0731684404037047&rft_dat=%3Cproquest_cross%3E28255216%3C/proquest_cross%3E%3Curl%3E%3C/url%3E&disable_directlink=true&sfx.directlink=off&sfx.report_link=0&rft_id=info:oai/&rft_pqid=28255216&rft_id=info:pmid/&rft_sage_id=10.1177_0731684404037047&rfr_iscdi=true |