Non-Uniform Finite Strip Method for Flexed Composite Plates
This article presents a new non-uniform finite strip technique for analyz ing composite laminates having both material and geometrically non-uniform cross sec tions. This is an extension of the conventional concept of the finite strip method which deals with uniform cross sections only. The applicat...
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| Veröffentlicht in: | Journal of composite materials 1993, Vol.27 (4), p.332-351 |
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| container_end_page | 351 |
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| container_issue | 4 |
| container_start_page | 332 |
| container_title | Journal of composite materials |
| container_volume | 27 |
| creator | Avrashi, J. Lin, C.H. Rauch, B.J. Rhee, J. Rowlands, R.E. |
| description | This article presents a new non-uniform finite strip technique for analyz ing composite laminates having both material and geometrically non-uniform cross sec tions. This is an extension of the conventional concept of the finite strip method which deals with uniform cross sections only. The application of the proposed method for flexed composite plates is illustrated. Numerical results are demonstrated for a transversely loaded circular composite plate containing an eccentric hole and are compared with those from an independent finite element analysis and with measured data. The spectral conver gence characteristics of the non-uniform strips are discussed, and the enhanced accuracy and reduced computer efforts are compared with those for the conventional finite element method. |
| doi_str_mv | 10.1177/002199839302700401 |
| format | Article |
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This is an extension of the conventional concept of the finite strip method which deals with uniform cross sections only. The application of the proposed method for flexed composite plates is illustrated. Numerical results are demonstrated for a transversely loaded circular composite plate containing an eccentric hole and are compared with those from an independent finite element analysis and with measured data. 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This is an extension of the conventional concept of the finite strip method which deals with uniform cross sections only. The application of the proposed method for flexed composite plates is illustrated. Numerical results are demonstrated for a transversely loaded circular composite plate containing an eccentric hole and are compared with those from an independent finite element analysis and with measured data. The spectral conver gence characteristics of the non-uniform strips are discussed, and the enhanced accuracy and reduced computer efforts are compared with those for the conventional finite element method.</description><subject>360603 - Materials- Properties</subject><subject>990200 - Mathematics & Computers</subject><subject>CALCULATION METHODS</subject><subject>COMPARATIVE EVALUATIONS</subject><subject>COMPOSITE MATERIALS</subject><subject>DOPPLER EFFECT</subject><subject>DYNAMIC LOADS</subject><subject>EVALUATION</subject><subject>Exact sciences and technology</subject><subject>FINITE ELEMENT METHOD</subject><subject>Fundamental areas of phenomenology (including applications)</subject><subject>GENERAL AND MISCELLANEOUS//MATHEMATICS, COMPUTING, AND INFORMATION SCIENCE</subject><subject>INTERFEROMETRY</subject><subject>MATERIALS</subject><subject>MATERIALS SCIENCE</subject><subject>NUMERICAL SOLUTION</subject><subject>Physics</subject><subject>PLATES</subject><subject>Solid mechanics</subject><subject>Static elasticity (thermoelasticity...)</subject><subject>STRESS ANALYSIS</subject><subject>STRESS INTENSITY FACTORS</subject><subject>Structural and continuum mechanics</subject><issn>0021-9983</issn><issn>1530-793X</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>1993</creationdate><recordtype>article</recordtype><recordid>eNqF0U1LxDAQBuAgCq6rf8BTEfFWd_LRpMGTLK4K6wfogreQTVO3S7epSRf035tS8SK4pznMMy_DDEKnGC4xFmICQLCUOZUUiABggPfQCGcUUiHp2z4a9SDtxSE6CmENAAIzPkJXj65JF01VOr9JZlVTdTZ56XzVJg-2W7kiiY1kVttPWyRTt2ld6MVzrTsbjtFBqetgT37qGC1mN6_Tu3T-dHs_vZ6nhjLZpVmOtRQ5ZpIV3IIsOZc5lAIbSkVOJBUFNXbJiSlyykoQJCs0EyUsOeax0jE6G3Jd6CoVTNzArIxrGms6xYHljNOILgbUevextaFTmyoYW9e6sW4bFI1GEkp2QsIxZVzgnRDzjGZZPPkYkQEa70LwtlStrzbafykMqn-P-vueOHT-k66D0XXpdWOq8DvJuIzReWSTgQX9btXabX0TT_1f8DfVRpjC</recordid><startdate>1993</startdate><enddate>1993</enddate><creator>Avrashi, J.</creator><creator>Lin, C.H.</creator><creator>Rauch, B.J.</creator><creator>Rhee, J.</creator><creator>Rowlands, R.E.</creator><general>SAGE Publications</general><general>Technomic</general><scope>IQODW</scope><scope>AAYXX</scope><scope>CITATION</scope><scope>7SC</scope><scope>7SR</scope><scope>8FD</scope><scope>FR3</scope><scope>H8D</scope><scope>JG9</scope><scope>JQ2</scope><scope>KR7</scope><scope>L7M</scope><scope>L~C</scope><scope>L~D</scope><scope>OTOTI</scope></search><sort><creationdate>1993</creationdate><title>Non-Uniform Finite Strip Method for Flexed Composite Plates</title><author>Avrashi, J. ; Lin, C.H. ; Rauch, B.J. ; Rhee, J. ; Rowlands, R.E.</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-c349t-581a9781494d6e09f66980f71c33782937d3ceb62cd834f0725da47f0b61647f3</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>1993</creationdate><topic>360603 - Materials- Properties</topic><topic>990200 - Mathematics & Computers</topic><topic>CALCULATION METHODS</topic><topic>COMPARATIVE EVALUATIONS</topic><topic>COMPOSITE MATERIALS</topic><topic>DOPPLER EFFECT</topic><topic>DYNAMIC LOADS</topic><topic>EVALUATION</topic><topic>Exact sciences and technology</topic><topic>FINITE ELEMENT METHOD</topic><topic>Fundamental areas of phenomenology (including applications)</topic><topic>GENERAL AND MISCELLANEOUS//MATHEMATICS, COMPUTING, AND INFORMATION SCIENCE</topic><topic>INTERFEROMETRY</topic><topic>MATERIALS</topic><topic>MATERIALS SCIENCE</topic><topic>NUMERICAL SOLUTION</topic><topic>Physics</topic><topic>PLATES</topic><topic>Solid mechanics</topic><topic>Static elasticity (thermoelasticity...)</topic><topic>STRESS ANALYSIS</topic><topic>STRESS INTENSITY FACTORS</topic><topic>Structural and continuum mechanics</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Avrashi, J.</creatorcontrib><creatorcontrib>Lin, C.H.</creatorcontrib><creatorcontrib>Rauch, B.J.</creatorcontrib><creatorcontrib>Rhee, J.</creatorcontrib><creatorcontrib>Rowlands, R.E.</creatorcontrib><collection>Pascal-Francis</collection><collection>CrossRef</collection><collection>Computer and Information Systems Abstracts</collection><collection>Engineered Materials Abstracts</collection><collection>Technology Research Database</collection><collection>Engineering Research Database</collection><collection>Aerospace Database</collection><collection>Materials Research Database</collection><collection>ProQuest Computer Science Collection</collection><collection>Civil Engineering Abstracts</collection><collection>Advanced Technologies Database with Aerospace</collection><collection>Computer and Information Systems Abstracts Academic</collection><collection>Computer and Information Systems Abstracts Professional</collection><collection>OSTI.GOV</collection><jtitle>Journal of composite materials</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Avrashi, J.</au><au>Lin, C.H.</au><au>Rauch, B.J.</au><au>Rhee, J.</au><au>Rowlands, R.E.</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Non-Uniform Finite Strip Method for Flexed Composite Plates</atitle><jtitle>Journal of composite materials</jtitle><date>1993</date><risdate>1993</risdate><volume>27</volume><issue>4</issue><spage>332</spage><epage>351</epage><pages>332-351</pages><issn>0021-9983</issn><eissn>1530-793X</eissn><coden>JCOMBI</coden><abstract>This article presents a new non-uniform finite strip technique for analyz ing composite laminates having both material and geometrically non-uniform cross sec tions. This is an extension of the conventional concept of the finite strip method which deals with uniform cross sections only. The application of the proposed method for flexed composite plates is illustrated. Numerical results are demonstrated for a transversely loaded circular composite plate containing an eccentric hole and are compared with those from an independent finite element analysis and with measured data. The spectral conver gence characteristics of the non-uniform strips are discussed, and the enhanced accuracy and reduced computer efforts are compared with those for the conventional finite element method.</abstract><cop>Thousand Oaks, CA</cop><pub>SAGE Publications</pub><doi>10.1177/002199839302700401</doi><tpages>20</tpages></addata></record> |
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| ispartof | Journal of composite materials, 1993, Vol.27 (4), p.332-351 |
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| subjects | 360603 - Materials- Properties 990200 - Mathematics & Computers CALCULATION METHODS COMPARATIVE EVALUATIONS COMPOSITE MATERIALS DOPPLER EFFECT DYNAMIC LOADS EVALUATION Exact sciences and technology FINITE ELEMENT METHOD Fundamental areas of phenomenology (including applications) GENERAL AND MISCELLANEOUS//MATHEMATICS, COMPUTING, AND INFORMATION SCIENCE INTERFEROMETRY MATERIALS MATERIALS SCIENCE NUMERICAL SOLUTION Physics PLATES Solid mechanics Static elasticity (thermoelasticity...) STRESS ANALYSIS STRESS INTENSITY FACTORS Structural and continuum mechanics |
| title | Non-Uniform Finite Strip Method for Flexed Composite Plates |
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