A solid-shell transition element for geometrically non-linear analysis of laminated composite structures
Using the incremental equations of motion of a continuous medium and the total Lagrangian description, three different elements, i.e. degenerated shell element, 3‐D continuum element and solid‐shell transition element, are developed for the geometrically non‐linear analysis of laminated composite st...
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Veröffentlicht in: | International journal for numerical methods in engineering 1988-08, Vol.26 (8), p.1843-1854 |
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container_title | International journal for numerical methods in engineering |
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creator | Liao, C. L. Reddy, J. N. Engelstad, S. P. |
description | Using the incremental equations of motion of a continuous medium and the total Lagrangian description, three different elements, i.e. degenerated shell element, 3‐D continuum element and solid‐shell transition element, are developed for the geometrically non‐linear analysis of laminated composite structures. Compatibility and completeness requirements are stressed in modelling shell‐type structures in order to assure the convergence of the finite element analysis. A number of laminated plate and shell examples are presented to demonstrate the validity and efficiency of various elements. |
doi_str_mv | 10.1002/nme.1620260811 |
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L. ; Reddy, J. N. ; Engelstad, S. P.</creator><creatorcontrib>Liao, C. L. ; Reddy, J. N. ; Engelstad, S. P.</creatorcontrib><description>Using the incremental equations of motion of a continuous medium and the total Lagrangian description, three different elements, i.e. degenerated shell element, 3‐D continuum element and solid‐shell transition element, are developed for the geometrically non‐linear analysis of laminated composite structures. Compatibility and completeness requirements are stressed in modelling shell‐type structures in order to assure the convergence of the finite element analysis. A number of laminated plate and shell examples are presented to demonstrate the validity and efficiency of various elements.</description><identifier>ISSN: 0029-5981</identifier><identifier>EISSN: 1097-0207</identifier><identifier>DOI: 10.1002/nme.1620260811</identifier><identifier>CODEN: IJNMBH</identifier><language>eng</language><publisher>New York: John Wiley & Sons, Ltd</publisher><subject>composite materials ; Exact sciences and technology ; finite element method ; Fundamental areas of phenomenology (including applications) ; Physics ; shells ; Solid mechanics ; Static elasticity (thermoelasticity...) ; stress ; Structural and continuum mechanics</subject><ispartof>International journal for numerical methods in engineering, 1988-08, Vol.26 (8), p.1843-1854</ispartof><rights>Copyright © 1988 John Wiley & Sons, Ltd</rights><rights>1989 INIST-CNRS</rights><lds50>peer_reviewed</lds50><woscitedreferencessubscribed>false</woscitedreferencessubscribed><citedby>FETCH-LOGICAL-c4791-abfd10d89a9f64a12b5d0daed48889863616c8e05a9d71ab8f2dc6a5e76927fd3</citedby><cites>FETCH-LOGICAL-c4791-abfd10d89a9f64a12b5d0daed48889863616c8e05a9d71ab8f2dc6a5e76927fd3</cites></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><linktopdf>$$Uhttps://onlinelibrary.wiley.com/doi/pdf/10.1002%2Fnme.1620260811$$EPDF$$P50$$Gwiley$$H</linktopdf><linktohtml>$$Uhttps://onlinelibrary.wiley.com/doi/full/10.1002%2Fnme.1620260811$$EHTML$$P50$$Gwiley$$H</linktohtml><link.rule.ids>314,776,780,1411,27901,27902,45550,45551</link.rule.ids><backlink>$$Uhttp://pascal-francis.inist.fr/vibad/index.php?action=getRecordDetail&idt=7030248$$DView record in Pascal Francis$$Hfree_for_read</backlink></links><search><creatorcontrib>Liao, C. L.</creatorcontrib><creatorcontrib>Reddy, J. N.</creatorcontrib><creatorcontrib>Engelstad, S. P.</creatorcontrib><title>A solid-shell transition element for geometrically non-linear analysis of laminated composite structures</title><title>International journal for numerical methods in engineering</title><addtitle>Int. J. Numer. Meth. Engng</addtitle><description>Using the incremental equations of motion of a continuous medium and the total Lagrangian description, three different elements, i.e. degenerated shell element, 3‐D continuum element and solid‐shell transition element, are developed for the geometrically non‐linear analysis of laminated composite structures. Compatibility and completeness requirements are stressed in modelling shell‐type structures in order to assure the convergence of the finite element analysis. A number of laminated plate and shell examples are presented to demonstrate the validity and efficiency of various elements.</description><subject>composite materials</subject><subject>Exact sciences and technology</subject><subject>finite element method</subject><subject>Fundamental areas of phenomenology (including applications)</subject><subject>Physics</subject><subject>shells</subject><subject>Solid mechanics</subject><subject>Static elasticity (thermoelasticity...)</subject><subject>stress</subject><subject>Structural and continuum mechanics</subject><issn>0029-5981</issn><issn>1097-0207</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>1988</creationdate><recordtype>article</recordtype><recordid>eNqNkT1vFDEQhlcIJI5AS-0CQbWXsXf9VUZROIiOJFJAlJZvPUsMXvuw90Tu32N0UVAaQjXN876jmadpXlNYUgB2HCdcUsGACVCUPmkWFLRsgYF82iwqoFuuFX3evCjlOwClHLpFc3NCSgreteUGQyBztrH42adIMOCEcSZjyuQbpgnn7Acbwp7EFNvgI9pMbLRhX3whaSTBTj7aGR0Z0rRNtQZJmfNumHcZy8vm2WhDwVd386j58v7s8-mHdn25-nh6sm6HXmra2s3oKDilrR5FbynbcAfOouuVUlqJTlAxKARutZPUbtTI3CAsRyk0k6Prjpp3h95tTj93WGYz-TLU22zEtCtG9oJKrZis5Nt_kowD7Tnv_ges39X6cZBpWlVBBZcHcMiplIyj2WY_2bw3FMwfmabKNH9l1sCbu2ZbqoSxahp8uU9J6ID1qmL6gP3yAfePlJqLT2cPVrSHrC8z3t5nbf5hhOwkN18vVkZd8avVuVyb6-439xLAVA</recordid><startdate>198808</startdate><enddate>198808</enddate><creator>Liao, C. 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P.</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>A solid-shell transition element for geometrically non-linear analysis of laminated composite structures</atitle><jtitle>International journal for numerical methods in engineering</jtitle><addtitle>Int. J. Numer. Meth. Engng</addtitle><date>1988-08</date><risdate>1988</risdate><volume>26</volume><issue>8</issue><spage>1843</spage><epage>1854</epage><pages>1843-1854</pages><issn>0029-5981</issn><eissn>1097-0207</eissn><coden>IJNMBH</coden><abstract>Using the incremental equations of motion of a continuous medium and the total Lagrangian description, three different elements, i.e. degenerated shell element, 3‐D continuum element and solid‐shell transition element, are developed for the geometrically non‐linear analysis of laminated composite structures. Compatibility and completeness requirements are stressed in modelling shell‐type structures in order to assure the convergence of the finite element analysis. A number of laminated plate and shell examples are presented to demonstrate the validity and efficiency of various elements.</abstract><cop>New York</cop><pub>John Wiley & Sons, Ltd</pub><doi>10.1002/nme.1620260811</doi><tpages>12</tpages></addata></record> |
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subjects | composite materials Exact sciences and technology finite element method Fundamental areas of phenomenology (including applications) Physics shells Solid mechanics Static elasticity (thermoelasticity...) stress Structural and continuum mechanics |
title | A solid-shell transition element for geometrically non-linear analysis of laminated composite structures |
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