Multiobjective shape and material optimization of composite structures including damping
A multiobjective optimal design methodology is developed for lightweight, low-cost composite structures of improved dynamic performance. The design objectives may include minimization of damped resonance amplitudes (or maximization of modal damping), weight, and material cost. The design vector incl...
Gespeichert in:
Veröffentlicht in: | AIAA journal 1992-03, Vol.30 (3), p.805-813 |
---|---|
Hauptverfasser: | , |
Format: | Artikel |
Sprache: | eng |
Schlagworte: | |
Online-Zugang: | Volltext |
Tags: |
Tag hinzufügen
Keine Tags, Fügen Sie den ersten Tag hinzu!
|
container_end_page | 813 |
---|---|
container_issue | 3 |
container_start_page | 805 |
container_title | AIAA journal |
container_volume | 30 |
creator | Saravanos, D. A Chamis, C. C |
description | A multiobjective optimal design methodology is developed for lightweight, low-cost composite structures of improved dynamic performance. The design objectives may include minimization of damped resonance amplitudes (or maximization of modal damping), weight, and material cost. The design vector includes micromechanics, laminate, and structural shape parameters. Constraints are imposed on static displacements, static and dynamic ply stresses, dynamic amplitudes, and natural frequencies. The effects of composite damping tailoring on the dynamics of the composite structure are incorporated. Applications on a cantilever composite beam and plate illustrate that only the proposed multiobjective formulation as opposed to single objective functions, may simultaneously improve the objectives. The significance of composite damping in the design of advanced composite structures is also demonstrated, and the results indicate that the minimum-weight design or design methods based on undamped dynamics may fail to improve the dynamic performance near resonances. An HM-S/epoxy composite is discussed. |
doi_str_mv | 10.2514/3.10988 |
format | Article |
fullrecord | <record><control><sourceid>proquest_aiaa_</sourceid><recordid>TN_cdi_proquest_miscellaneous_25711204</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>25716307</sourcerecordid><originalsourceid>FETCH-LOGICAL-a499t-ad8fda4517286e73d03576c862fa611bef93227b96a6e24a33476a40598054083</originalsourceid><addsrcrecordid>eNqN0ctKw0AUBuBBFKxVfAEXWYjiInWuyWQpxRtU3Ch0N5wmE52SZOJcRH16U9NlF64Oh__jX5yD0CnBMyoIv2Yzggsp99CECMZSJsVyH00wxiQlXNBDdOT9ethoLskELZ9iE4xdrXUZzKdO_Dv0OoGuSloI2hloEtsH05ofGFiX2Dopbdtbb8KAg4tliE77xHRlEyvTvSUVtP0wj9FBDY3XJ9s5Ra93ty_zh3TxfP84v1mkwIsipFDJugIuSE5lpnNWYSbyrJQZrSEjZKXrglGar4oMMk05MMbzDDgWhcSCY8mm6GLs7Z39iNoH1Rpf6qaBTtvoFRU5yRjO_wWJlPx_kOINvBxh6az3Tteqd6YF960IVptfKKb-fjHIs1F24EF1wXlFioJizAVnZIjPxxgMgFrb6LrhZDtarnaxbaz6qlZ1bJqgvwL7BRbJnbY</addsrcrecordid><sourcetype>Aggregation Database</sourcetype><iscdi>true</iscdi><recordtype>article</recordtype><pqid>25711204</pqid></control><display><type>article</type><title>Multiobjective shape and material optimization of composite structures including damping</title><source>NASA Technical Reports Server</source><source>Alma/SFX Local Collection</source><creator>Saravanos, D. A ; Chamis, C. C</creator><creatorcontrib>Saravanos, D. A ; Chamis, C. C</creatorcontrib><description>A multiobjective optimal design methodology is developed for lightweight, low-cost composite structures of improved dynamic performance. The design objectives may include minimization of damped resonance amplitudes (or maximization of modal damping), weight, and material cost. The design vector includes micromechanics, laminate, and structural shape parameters. Constraints are imposed on static displacements, static and dynamic ply stresses, dynamic amplitudes, and natural frequencies. The effects of composite damping tailoring on the dynamics of the composite structure are incorporated. Applications on a cantilever composite beam and plate illustrate that only the proposed multiobjective formulation as opposed to single objective functions, may simultaneously improve the objectives. The significance of composite damping in the design of advanced composite structures is also demonstrated, and the results indicate that the minimum-weight design or design methods based on undamped dynamics may fail to improve the dynamic performance near resonances. An HM-S/epoxy composite is discussed.</description><identifier>ISSN: 0001-1452</identifier><identifier>EISSN: 1533-385X</identifier><identifier>DOI: 10.2514/3.10988</identifier><language>eng</language><publisher>Legacy CDMS</publisher><subject>Structural Mechanics</subject><ispartof>AIAA journal, 1992-03, Vol.30 (3), p.805-813</ispartof><lds50>peer_reviewed</lds50><oa>free_for_read</oa><woscitedreferencessubscribed>false</woscitedreferencessubscribed><citedby>FETCH-LOGICAL-a499t-ad8fda4517286e73d03576c862fa611bef93227b96a6e24a33476a40598054083</citedby><cites>FETCH-LOGICAL-a499t-ad8fda4517286e73d03576c862fa611bef93227b96a6e24a33476a40598054083</cites></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><link.rule.ids>314,780,784,27922,27923</link.rule.ids></links><search><creatorcontrib>Saravanos, D. A</creatorcontrib><creatorcontrib>Chamis, C. C</creatorcontrib><title>Multiobjective shape and material optimization of composite structures including damping</title><title>AIAA journal</title><description>A multiobjective optimal design methodology is developed for lightweight, low-cost composite structures of improved dynamic performance. The design objectives may include minimization of damped resonance amplitudes (or maximization of modal damping), weight, and material cost. The design vector includes micromechanics, laminate, and structural shape parameters. Constraints are imposed on static displacements, static and dynamic ply stresses, dynamic amplitudes, and natural frequencies. The effects of composite damping tailoring on the dynamics of the composite structure are incorporated. Applications on a cantilever composite beam and plate illustrate that only the proposed multiobjective formulation as opposed to single objective functions, may simultaneously improve the objectives. The significance of composite damping in the design of advanced composite structures is also demonstrated, and the results indicate that the minimum-weight design or design methods based on undamped dynamics may fail to improve the dynamic performance near resonances. An HM-S/epoxy composite is discussed.</description><subject>Structural Mechanics</subject><issn>0001-1452</issn><issn>1533-385X</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>1992</creationdate><recordtype>article</recordtype><sourceid>CYI</sourceid><recordid>eNqN0ctKw0AUBuBBFKxVfAEXWYjiInWuyWQpxRtU3Ch0N5wmE52SZOJcRH16U9NlF64Oh__jX5yD0CnBMyoIv2Yzggsp99CECMZSJsVyH00wxiQlXNBDdOT9ethoLskELZ9iE4xdrXUZzKdO_Dv0OoGuSloI2hloEtsH05ofGFiX2Dopbdtbb8KAg4tliE77xHRlEyvTvSUVtP0wj9FBDY3XJ9s5Ra93ty_zh3TxfP84v1mkwIsipFDJugIuSE5lpnNWYSbyrJQZrSEjZKXrglGar4oMMk05MMbzDDgWhcSCY8mm6GLs7Z39iNoH1Rpf6qaBTtvoFRU5yRjO_wWJlPx_kOINvBxh6az3Tteqd6YF960IVptfKKb-fjHIs1F24EF1wXlFioJizAVnZIjPxxgMgFrb6LrhZDtarnaxbaz6qlZ1bJqgvwL7BRbJnbY</recordid><startdate>19920301</startdate><enddate>19920301</enddate><creator>Saravanos, D. A</creator><creator>Chamis, C. C</creator><scope>CYE</scope><scope>CYI</scope><scope>AAYXX</scope><scope>CITATION</scope><scope>8FD</scope><scope>FR3</scope><scope>KR7</scope><scope>7SR</scope><scope>JG9</scope><scope>H8D</scope><scope>L7M</scope></search><sort><creationdate>19920301</creationdate><title>Multiobjective shape and material optimization of composite structures including damping</title><author>Saravanos, D. A ; Chamis, C. C</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-a499t-ad8fda4517286e73d03576c862fa611bef93227b96a6e24a33476a40598054083</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>1992</creationdate><topic>Structural Mechanics</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Saravanos, D. A</creatorcontrib><creatorcontrib>Chamis, C. C</creatorcontrib><collection>NASA Scientific and Technical Information</collection><collection>NASA Technical Reports Server</collection><collection>CrossRef</collection><collection>Technology Research Database</collection><collection>Engineering Research Database</collection><collection>Civil Engineering Abstracts</collection><collection>Engineered Materials Abstracts</collection><collection>Materials 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>Saravanos, D. A</au><au>Chamis, C. C</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Multiobjective shape and material optimization of composite structures including damping</atitle><jtitle>AIAA journal</jtitle><date>1992-03-01</date><risdate>1992</risdate><volume>30</volume><issue>3</issue><spage>805</spage><epage>813</epage><pages>805-813</pages><issn>0001-1452</issn><eissn>1533-385X</eissn><abstract>A multiobjective optimal design methodology is developed for lightweight, low-cost composite structures of improved dynamic performance. The design objectives may include minimization of damped resonance amplitudes (or maximization of modal damping), weight, and material cost. The design vector includes micromechanics, laminate, and structural shape parameters. Constraints are imposed on static displacements, static and dynamic ply stresses, dynamic amplitudes, and natural frequencies. The effects of composite damping tailoring on the dynamics of the composite structure are incorporated. Applications on a cantilever composite beam and plate illustrate that only the proposed multiobjective formulation as opposed to single objective functions, may simultaneously improve the objectives. The significance of composite damping in the design of advanced composite structures is also demonstrated, and the results indicate that the minimum-weight design or design methods based on undamped dynamics may fail to improve the dynamic performance near resonances. An HM-S/epoxy composite is discussed.</abstract><cop>Legacy CDMS</cop><doi>10.2514/3.10988</doi><tpages>9</tpages><oa>free_for_read</oa></addata></record> |
fulltext | fulltext |
identifier | ISSN: 0001-1452 |
ispartof | AIAA journal, 1992-03, Vol.30 (3), p.805-813 |
issn | 0001-1452 1533-385X |
language | eng |
recordid | cdi_proquest_miscellaneous_25711204 |
source | NASA Technical Reports Server; Alma/SFX Local Collection |
subjects | Structural Mechanics |
title | Multiobjective shape and material optimization of composite structures including damping |
url | https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-01-14T07%3A48%3A00IST&url_ver=Z39.88-2004&url_ctx_fmt=infofi/fmt:kev:mtx:ctx&rfr_id=info:sid/primo.exlibrisgroup.com:primo3-Article-proquest_aiaa_&rft_val_fmt=info:ofi/fmt:kev:mtx:journal&rft.genre=article&rft.atitle=Multiobjective%20shape%20and%20material%20optimization%20of%20composite%20structures%20including%20damping&rft.jtitle=AIAA%20journal&rft.au=Saravanos,%20D.%20A&rft.date=1992-03-01&rft.volume=30&rft.issue=3&rft.spage=805&rft.epage=813&rft.pages=805-813&rft.issn=0001-1452&rft.eissn=1533-385X&rft_id=info:doi/10.2514/3.10988&rft_dat=%3Cproquest_aiaa_%3E25716307%3C/proquest_aiaa_%3E%3Curl%3E%3C/url%3E&disable_directlink=true&sfx.directlink=off&sfx.report_link=0&rft_id=info:oai/&rft_pqid=25711204&rft_id=info:pmid/&rfr_iscdi=true |