Dynamic Response Analysis of Bird Strike on Aircraft Windshield Based on Damage-modified Nonlinear Viscoelastic Constitutive Relation
Damage-modified nonlinear viscoelastic constitutive equation and failure criterion are introduced and the three-dimensional incremental forms are deduced based on the updated Lagrangian approach. A simple tensile test model and a split Hopkinson pressure bar model are built to verify the accuracy of...
Gespeichert in:
| Veröffentlicht in: | Chinese journal of aeronautics 2007-12, Vol.20 (6), p.511-517 |
|---|---|
| Hauptverfasser: | , , , |
| Format: | Artikel |
| Sprache: | eng |
| Schlagworte: | |
| Online-Zugang: | Volltext |
| Tags: |
Tag hinzufügen
Keine Tags, Fügen Sie den ersten Tag hinzu!
|
| container_end_page | 517 |
|---|---|
| container_issue | 6 |
| container_start_page | 511 |
| container_title | Chinese journal of aeronautics |
| container_volume | 20 |
| creator | Xinjun, Wang Zhenzhou, Feng Fusheng, Wang Zhufeng, Yue |
| description | Damage-modified nonlinear viscoelastic constitutive equation and failure criterion are introduced and the three-dimensional incremental forms are deduced based on the updated Lagrangian approach. A simple tensile test model and a split Hopkinson pressure bar model are built to verify the accuracy of the subroutine implemented within the non-linear finite element program LS-DYNA. A numerical model of bird strike on windshield is established to study the responses of windshield under three different bird velocities at three sites. The bird is represented by a cylinder with a hemisphere at each end and the contact-impact coupling algorithm is used in this study. It is found that the implemented subroutine can properly describe the mechanical behavior of polymethyl methaerylate under low and high strain rates and large deformation, and can be used validly. |
| doi_str_mv | 10.1016/S1000-9361(07)60075-2 |
| format | Article |
| fullrecord | <record><control><sourceid>wanfang_jour_proqu</sourceid><recordid>TN_cdi_wanfang_journals_hkxb_e200706005</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><cqvip_id>26066539</cqvip_id><wanfj_id>hkxb_e200706005</wanfj_id><els_id>S1000936107600752</els_id><sourcerecordid>hkxb_e200706005</sourcerecordid><originalsourceid>FETCH-LOGICAL-c446t-d4dd499dec9f9d234922d40b255db66e6bad83d2d66291d9c107ee080bba79163</originalsourceid><addsrcrecordid>eNqFUctuFDEQnANICYFPQLI4ADkM-DHjWZ_QZsNLioJEeBwtj92z29kZe2N7Q_YD-G-82YhrTi11V3WpqqrqJaPvGGXy_RWjlNZKSPaWdqeS0q6t-ZPq-P_6qHqW0jWlQnWMHld_z3feTGjJd0ib4BOQuTfjLmEiYSBnGB25yhHXQIInc4w2miGT3-hdWiGMjpyZBG5_PDeTWUI9BYcDltVl8CN6MJH8wmQDjCblorMoIhnzNuMtFNHRZAz-efV0MGOCFw_zpPr56eOPxZf64tvnr4v5RW2bRubaNc41SjmwalCOi0Zx7hra87Z1vZQge-NmwnEnJVfMKctoB0BntO9Np5gUJ9Wbw98_xg_GL_V12MbiN-nV-q7XwEtetITWFuTrA3ITw80WUtZTcQHjaDyEbdKCsU6omSjA9gC0MaQUYdCbiJOJO82o3lei7yvR--w17fR9JZoX3ocDD4rfW4Sok0XwFhxGsFm7gI9-ePWgvAp-eYPFTm_sesARNJdUylYo8Q_z76I1</addsrcrecordid><sourcetype>Aggregation Database</sourcetype><iscdi>true</iscdi><recordtype>article</recordtype><pqid>31173983</pqid></control><display><type>article</type><title>Dynamic Response Analysis of Bird Strike on Aircraft Windshield Based on Damage-modified Nonlinear Viscoelastic Constitutive Relation</title><source>Elsevier ScienceDirect Journals</source><source>Elektronische Zeitschriftenbibliothek - Frei zugängliche E-Journals</source><creator>Xinjun, Wang ; Zhenzhou, Feng ; Fusheng, Wang ; Zhufeng, Yue</creator><creatorcontrib>Xinjun, Wang ; Zhenzhou, Feng ; Fusheng, Wang ; Zhufeng, Yue</creatorcontrib><description>Damage-modified nonlinear viscoelastic constitutive equation and failure criterion are introduced and the three-dimensional incremental forms are deduced based on the updated Lagrangian approach. A simple tensile test model and a split Hopkinson pressure bar model are built to verify the accuracy of the subroutine implemented within the non-linear finite element program LS-DYNA. A numerical model of bird strike on windshield is established to study the responses of windshield under three different bird velocities at three sites. The bird is represented by a cylinder with a hemisphere at each end and the contact-impact coupling algorithm is used in this study. It is found that the implemented subroutine can properly describe the mechanical behavior of polymethyl methaerylate under low and high strain rates and large deformation, and can be used validly.</description><identifier>ISSN: 1000-9361</identifier><identifier>DOI: 10.1016/S1000-9361(07)60075-2</identifier><language>eng</language><publisher>Elsevier Ltd</publisher><subject>bird strike ; damage-modified non-linear viscoelastic constitutive relation ; material subroutine ; strain rate ; windshield ; 挡风玻璃 ; 物质子程序 ; 非线性粘弹性构成 ; 飞机事故</subject><ispartof>Chinese journal of aeronautics, 2007-12, Vol.20 (6), p.511-517</ispartof><rights>2007 Chinese Journal of Aeronautics</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-c446t-d4dd499dec9f9d234922d40b255db66e6bad83d2d66291d9c107ee080bba79163</citedby><cites>FETCH-LOGICAL-c446t-d4dd499dec9f9d234922d40b255db66e6bad83d2d66291d9c107ee080bba79163</cites></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Uhttp://image.cqvip.com/vip1000/qk/83889X/83889X.jpg</thumbnail><linktohtml>$$Uhttps://www.sciencedirect.com/science/article/pii/S1000936107600752$$EHTML$$P50$$Gelsevier$$Hfree_for_read</linktohtml><link.rule.ids>314,776,780,3536,27903,27904,65309</link.rule.ids></links><search><creatorcontrib>Xinjun, Wang</creatorcontrib><creatorcontrib>Zhenzhou, Feng</creatorcontrib><creatorcontrib>Fusheng, Wang</creatorcontrib><creatorcontrib>Zhufeng, Yue</creatorcontrib><title>Dynamic Response Analysis of Bird Strike on Aircraft Windshield Based on Damage-modified Nonlinear Viscoelastic Constitutive Relation</title><title>Chinese journal of aeronautics</title><addtitle>Chinese Journal of Aeronautics</addtitle><description>Damage-modified nonlinear viscoelastic constitutive equation and failure criterion are introduced and the three-dimensional incremental forms are deduced based on the updated Lagrangian approach. A simple tensile test model and a split Hopkinson pressure bar model are built to verify the accuracy of the subroutine implemented within the non-linear finite element program LS-DYNA. A numerical model of bird strike on windshield is established to study the responses of windshield under three different bird velocities at three sites. The bird is represented by a cylinder with a hemisphere at each end and the contact-impact coupling algorithm is used in this study. It is found that the implemented subroutine can properly describe the mechanical behavior of polymethyl methaerylate under low and high strain rates and large deformation, and can be used validly.</description><subject>bird strike</subject><subject>damage-modified non-linear viscoelastic constitutive relation</subject><subject>material subroutine</subject><subject>strain rate</subject><subject>windshield</subject><subject>挡风玻璃</subject><subject>物质子程序</subject><subject>非线性粘弹性构成</subject><subject>飞机事故</subject><issn>1000-9361</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2007</creationdate><recordtype>article</recordtype><recordid>eNqFUctuFDEQnANICYFPQLI4ADkM-DHjWZ_QZsNLioJEeBwtj92z29kZe2N7Q_YD-G-82YhrTi11V3WpqqrqJaPvGGXy_RWjlNZKSPaWdqeS0q6t-ZPq-P_6qHqW0jWlQnWMHld_z3feTGjJd0ib4BOQuTfjLmEiYSBnGB25yhHXQIInc4w2miGT3-hdWiGMjpyZBG5_PDeTWUI9BYcDltVl8CN6MJH8wmQDjCblorMoIhnzNuMtFNHRZAz-efV0MGOCFw_zpPr56eOPxZf64tvnr4v5RW2bRubaNc41SjmwalCOi0Zx7hra87Z1vZQge-NmwnEnJVfMKctoB0BntO9Np5gUJ9Wbw98_xg_GL_V12MbiN-nV-q7XwEtetITWFuTrA3ITw80WUtZTcQHjaDyEbdKCsU6omSjA9gC0MaQUYdCbiJOJO82o3lei7yvR--w17fR9JZoX3ocDD4rfW4Sok0XwFhxGsFm7gI9-ePWgvAp-eYPFTm_sesARNJdUylYo8Q_z76I1</recordid><startdate>20071201</startdate><enddate>20071201</enddate><creator>Xinjun, Wang</creator><creator>Zhenzhou, Feng</creator><creator>Fusheng, Wang</creator><creator>Zhufeng, Yue</creator><general>Elsevier Ltd</general><general>Department of Engineering Mechanics, Northwestern Polytechnical University, Xi'an 710072, China</general><scope>2RA</scope><scope>92L</scope><scope>CQIGP</scope><scope>W92</scope><scope>~WA</scope><scope>6I.</scope><scope>AAFTH</scope><scope>AAYXX</scope><scope>CITATION</scope><scope>7TB</scope><scope>8FD</scope><scope>FR3</scope><scope>H8D</scope><scope>L7M</scope><scope>2B.</scope><scope>4A8</scope><scope>92I</scope><scope>93N</scope><scope>PSX</scope><scope>TCJ</scope></search><sort><creationdate>20071201</creationdate><title>Dynamic Response Analysis of Bird Strike on Aircraft Windshield Based on Damage-modified Nonlinear Viscoelastic Constitutive Relation</title><author>Xinjun, Wang ; Zhenzhou, Feng ; Fusheng, Wang ; Zhufeng, Yue</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-c446t-d4dd499dec9f9d234922d40b255db66e6bad83d2d66291d9c107ee080bba79163</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2007</creationdate><topic>bird strike</topic><topic>damage-modified non-linear viscoelastic constitutive relation</topic><topic>material subroutine</topic><topic>strain rate</topic><topic>windshield</topic><topic>挡风玻璃</topic><topic>物质子程序</topic><topic>非线性粘弹性构成</topic><topic>飞机事故</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Xinjun, Wang</creatorcontrib><creatorcontrib>Zhenzhou, Feng</creatorcontrib><creatorcontrib>Fusheng, Wang</creatorcontrib><creatorcontrib>Zhufeng, Yue</creatorcontrib><collection>中文科技期刊数据库</collection><collection>中文科技期刊数据库-CALIS站点</collection><collection>中文科技期刊数据库-7.0平台</collection><collection>中文科技期刊数据库-工程技术</collection><collection>中文科技期刊数据库- 镜像站点</collection><collection>ScienceDirect Open Access Titles</collection><collection>Elsevier:ScienceDirect:Open Access</collection><collection>CrossRef</collection><collection>Mechanical & Transportation Engineering Abstracts</collection><collection>Technology Research Database</collection><collection>Engineering Research Database</collection><collection>Aerospace Database</collection><collection>Advanced Technologies Database with Aerospace</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>Xinjun, Wang</au><au>Zhenzhou, Feng</au><au>Fusheng, Wang</au><au>Zhufeng, Yue</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Dynamic Response Analysis of Bird Strike on Aircraft Windshield Based on Damage-modified Nonlinear Viscoelastic Constitutive Relation</atitle><jtitle>Chinese journal of aeronautics</jtitle><addtitle>Chinese Journal of Aeronautics</addtitle><date>2007-12-01</date><risdate>2007</risdate><volume>20</volume><issue>6</issue><spage>511</spage><epage>517</epage><pages>511-517</pages><issn>1000-9361</issn><abstract>Damage-modified nonlinear viscoelastic constitutive equation and failure criterion are introduced and the three-dimensional incremental forms are deduced based on the updated Lagrangian approach. A simple tensile test model and a split Hopkinson pressure bar model are built to verify the accuracy of the subroutine implemented within the non-linear finite element program LS-DYNA. A numerical model of bird strike on windshield is established to study the responses of windshield under three different bird velocities at three sites. The bird is represented by a cylinder with a hemisphere at each end and the contact-impact coupling algorithm is used in this study. It is found that the implemented subroutine can properly describe the mechanical behavior of polymethyl methaerylate under low and high strain rates and large deformation, and can be used validly.</abstract><pub>Elsevier Ltd</pub><doi>10.1016/S1000-9361(07)60075-2</doi><tpages>7</tpages><oa>free_for_read</oa></addata></record> |
| fulltext | fulltext |
| identifier | ISSN: 1000-9361 |
| ispartof | Chinese journal of aeronautics, 2007-12, Vol.20 (6), p.511-517 |
| issn | 1000-9361 |
| language | eng |
| recordid | cdi_wanfang_journals_hkxb_e200706005 |
| source | Elsevier ScienceDirect Journals; Elektronische Zeitschriftenbibliothek - Frei zugängliche E-Journals |
| subjects | bird strike damage-modified non-linear viscoelastic constitutive relation material subroutine strain rate windshield 挡风玻璃 物质子程序 非线性粘弹性构成 飞机事故 |
| title | Dynamic Response Analysis of Bird Strike on Aircraft Windshield Based on Damage-modified Nonlinear Viscoelastic Constitutive Relation |
| url | https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-01-25T21%3A14%3A41IST&url_ver=Z39.88-2004&url_ctx_fmt=infofi/fmt:kev:mtx:ctx&rfr_id=info:sid/primo.exlibrisgroup.com:primo3-Article-wanfang_jour_proqu&rft_val_fmt=info:ofi/fmt:kev:mtx:journal&rft.genre=article&rft.atitle=Dynamic%20Response%20Analysis%20of%20Bird%20Strike%20on%20Aircraft%20Windshield%20Based%20on%20Damage-modified%20Nonlinear%20Viscoelastic%20Constitutive%20Relation&rft.jtitle=Chinese%20journal%20of%20aeronautics&rft.au=Xinjun,%20Wang&rft.date=2007-12-01&rft.volume=20&rft.issue=6&rft.spage=511&rft.epage=517&rft.pages=511-517&rft.issn=1000-9361&rft_id=info:doi/10.1016/S1000-9361(07)60075-2&rft_dat=%3Cwanfang_jour_proqu%3Ehkxb_e200706005%3C/wanfang_jour_proqu%3E%3Curl%3E%3C/url%3E&disable_directlink=true&sfx.directlink=off&sfx.report_link=0&rft_id=info:oai/&rft_pqid=31173983&rft_id=info:pmid/&rft_cqvip_id=26066539&rft_wanfj_id=hkxb_e200706005&rft_els_id=S1000936107600752&rfr_iscdi=true |