Dynamic response of honeycomb-FGS shells subjected to the dynamic loading using non-polynomial higher-order IGA
The main goal of this study is to use higher-order isogeometric analysis (IGA) to study the dynamic response of sandwich shells with an auxetic honeycomb core and two different functionally graded materials (FGM) skin layers (namely honeycomb-FGS shells) subjected to dynamic loading. Touratier'...
Gespeichert in:
| Veröffentlicht in: | Defence technology 2024-07, Vol.37, p.149-161 |
|---|---|
| Hauptverfasser: | , |
| Format: | Artikel |
| Sprache: | eng |
| Schlagworte: | |
| Online-Zugang: | Volltext |
| Tags: |
Tag hinzufügen
Keine Tags, Fügen Sie den ersten Tag hinzu!
|
| container_end_page | 161 |
|---|---|
| container_issue | |
| container_start_page | 149 |
| container_title | Defence technology |
| container_volume | 37 |
| creator | Le, Pham Binh Tran, Trung-Thanh |
| description | The main goal of this study is to use higher-order isogeometric analysis (IGA) to study the dynamic response of sandwich shells with an auxetic honeycomb core and two different functionally graded materials (FGM) skin layers (namely honeycomb-FGS shells) subjected to dynamic loading. Touratier's non-polynomial higher-order shear deformation theory (HSDT) is used due to its simplicity and performance. The governing equation is derived from Hamilton's principle. After verifying the present approach, the effect of input parameters on the dynamic response of honeycomb-FGS shells is carried out in detail. |
| doi_str_mv | 10.1016/j.dt.2023.12.002 |
| format | Article |
| fullrecord | <record><control><sourceid>proquest_cross</sourceid><recordid>TN_cdi_proquest_journals_3084907487</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><els_id>S2214914723003252</els_id><sourcerecordid>3084907487</sourcerecordid><originalsourceid>FETCH-LOGICAL-c317t-3a9505c8c642ba1712f814de8d046598dfb441c19a2dca0380dc2dc59526ce73</originalsourceid><addsrcrecordid>eNp1kL1rwzAQxU1poaHN3lHQ2a4ky1_dQtqkgUCHZheydI5lbMmV7IL_-9okQ5cud4_jvbvjFwRPBEcEk_SlidQQUUzjiNAIY3oTrCglLCwIy27_6Ptg7X2DMSb5PEuyVWDfJiM6LZED31vjAdkK1dbAJG1Xhrv9F_I1tK1HfiwbkAMoNFg01IDUNdlaobQ5o9Ev1VgT9radjO20aFGtzzW40DoFDh32m8fgrhKth_W1PwSn3ftp-xEeP_eH7eYYyphkQxiLIsGJzGXKaClIRmiVE6YgV5ilSZGrqmSMSFIIqqTAcY6VnFVSJDSVkMUPwfNlbe_s9wh-4I0dnZkv8hjnrMAZyxcXvriks947qHjvdCfcxAnmC1jecDXwBSwnlM9g58jrJQLz8z8aHPdSg5GgtJvpcGX1_-Ff38Z_-Q</addsrcrecordid><sourcetype>Aggregation Database</sourcetype><iscdi>true</iscdi><recordtype>article</recordtype><pqid>3084907487</pqid></control><display><type>article</type><title>Dynamic response of honeycomb-FGS shells subjected to the dynamic loading using non-polynomial higher-order IGA</title><source>ProQuest One Community College</source><source>ProQuest Central (Alumni Edition)</source><source>DOAJ Directory of Open Access Journals</source><source>ProQuest Central Korea</source><source>EZB-FREE-00999 freely available EZB journals</source><source>ProQuest Central UK/Ireland</source><source>Alma/SFX Local Collection</source><source>ProQuest Central</source><creator>Le, Pham Binh ; Tran, Trung-Thanh</creator><creatorcontrib>Le, Pham Binh ; Tran, Trung-Thanh</creatorcontrib><description>The main goal of this study is to use higher-order isogeometric analysis (IGA) to study the dynamic response of sandwich shells with an auxetic honeycomb core and two different functionally graded materials (FGM) skin layers (namely honeycomb-FGS shells) subjected to dynamic loading. Touratier's non-polynomial higher-order shear deformation theory (HSDT) is used due to its simplicity and performance. The governing equation is derived from Hamilton's principle. After verifying the present approach, the effect of input parameters on the dynamic response of honeycomb-FGS shells is carried out in detail.</description><identifier>ISSN: 2214-9147</identifier><identifier>ISSN: 2096-3459</identifier><identifier>EISSN: 2214-9147</identifier><identifier>DOI: 10.1016/j.dt.2023.12.002</identifier><language>eng</language><publisher>Beijing: Elsevier B.V</publisher><subject>Auxetic honeycomb ; Boundary conditions ; Composite materials ; Deformation effects ; Dynamic loads ; Dynamic response ; Elastic foundation ; FGM ; Functionally gradient materials ; Hamilton's principle ; Honeycomb cores ; IGA ; Mechanical properties ; Polynomials ; Shear deformation ; Shell ; Shells</subject><ispartof>Defence technology, 2024-07, Vol.37, p.149-161</ispartof><rights>2023 China Ordnance Society</rights><rights>2024. This work is published under http://creativecommons.org/licenses/by-nc-nd/4.0/ (the “License”). Notwithstanding the ProQuest Terms and Conditions, you may use this content in accordance with the terms of the License.</rights><lds50>peer_reviewed</lds50><oa>free_for_read</oa><woscitedreferencessubscribed>false</woscitedreferencessubscribed><cites>FETCH-LOGICAL-c317t-3a9505c8c642ba1712f814de8d046598dfb441c19a2dca0380dc2dc59526ce73</cites><orcidid>0000-0002-1730-0590</orcidid></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><linktohtml>$$Uhttps://www.proquest.com/docview/3084907487?pq-origsite=primo$$EHTML$$P50$$Gproquest$$Hfree_for_read</linktohtml><link.rule.ids>314,780,784,864,21388,21389,21391,27924,27925,33530,33744,34005,43659,43805,43953,64385,64389,72469,73128,73129,73131</link.rule.ids></links><search><creatorcontrib>Le, Pham Binh</creatorcontrib><creatorcontrib>Tran, Trung-Thanh</creatorcontrib><title>Dynamic response of honeycomb-FGS shells subjected to the dynamic loading using non-polynomial higher-order IGA</title><title>Defence technology</title><description>The main goal of this study is to use higher-order isogeometric analysis (IGA) to study the dynamic response of sandwich shells with an auxetic honeycomb core and two different functionally graded materials (FGM) skin layers (namely honeycomb-FGS shells) subjected to dynamic loading. Touratier's non-polynomial higher-order shear deformation theory (HSDT) is used due to its simplicity and performance. The governing equation is derived from Hamilton's principle. After verifying the present approach, the effect of input parameters on the dynamic response of honeycomb-FGS shells is carried out in detail.</description><subject>Auxetic honeycomb</subject><subject>Boundary conditions</subject><subject>Composite materials</subject><subject>Deformation effects</subject><subject>Dynamic loads</subject><subject>Dynamic response</subject><subject>Elastic foundation</subject><subject>FGM</subject><subject>Functionally gradient materials</subject><subject>Hamilton's principle</subject><subject>Honeycomb cores</subject><subject>IGA</subject><subject>Mechanical properties</subject><subject>Polynomials</subject><subject>Shear deformation</subject><subject>Shell</subject><subject>Shells</subject><issn>2214-9147</issn><issn>2096-3459</issn><issn>2214-9147</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2024</creationdate><recordtype>article</recordtype><sourceid>ABUWG</sourceid><sourceid>AFKRA</sourceid><sourceid>AZQEC</sourceid><sourceid>BENPR</sourceid><sourceid>CCPQU</sourceid><sourceid>DWQXO</sourceid><recordid>eNp1kL1rwzAQxU1poaHN3lHQ2a4ky1_dQtqkgUCHZheydI5lbMmV7IL_-9okQ5cud4_jvbvjFwRPBEcEk_SlidQQUUzjiNAIY3oTrCglLCwIy27_6Ptg7X2DMSb5PEuyVWDfJiM6LZED31vjAdkK1dbAJG1Xhrv9F_I1tK1HfiwbkAMoNFg01IDUNdlaobQ5o9Ev1VgT9radjO20aFGtzzW40DoFDh32m8fgrhKth_W1PwSn3ftp-xEeP_eH7eYYyphkQxiLIsGJzGXKaClIRmiVE6YgV5ilSZGrqmSMSFIIqqTAcY6VnFVSJDSVkMUPwfNlbe_s9wh-4I0dnZkv8hjnrMAZyxcXvriks947qHjvdCfcxAnmC1jecDXwBSwnlM9g58jrJQLz8z8aHPdSg5GgtJvpcGX1_-Ff38Z_-Q</recordid><startdate>20240701</startdate><enddate>20240701</enddate><creator>Le, Pham Binh</creator><creator>Tran, Trung-Thanh</creator><general>Elsevier B.V</general><general>KeAi Publishing Communications Ltd</general><scope>6I.</scope><scope>AAFTH</scope><scope>AAYXX</scope><scope>CITATION</scope><scope>3V.</scope><scope>7XB</scope><scope>88F</scope><scope>8FE</scope><scope>8FG</scope><scope>8FK</scope><scope>ABJCF</scope><scope>ABUWG</scope><scope>AFKRA</scope><scope>AZQEC</scope><scope>BENPR</scope><scope>BGLVJ</scope><scope>CCPQU</scope><scope>DWQXO</scope><scope>HCIFZ</scope><scope>L6V</scope><scope>M1Q</scope><scope>M7S</scope><scope>PIMPY</scope><scope>PQEST</scope><scope>PQQKQ</scope><scope>PQUKI</scope><scope>PRINS</scope><scope>PTHSS</scope><scope>Q9U</scope><orcidid>https://orcid.org/0000-0002-1730-0590</orcidid></search><sort><creationdate>20240701</creationdate><title>Dynamic response of honeycomb-FGS shells subjected to the dynamic loading using non-polynomial higher-order IGA</title><author>Le, Pham Binh ; Tran, Trung-Thanh</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-c317t-3a9505c8c642ba1712f814de8d046598dfb441c19a2dca0380dc2dc59526ce73</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2024</creationdate><topic>Auxetic honeycomb</topic><topic>Boundary conditions</topic><topic>Composite materials</topic><topic>Deformation effects</topic><topic>Dynamic loads</topic><topic>Dynamic response</topic><topic>Elastic foundation</topic><topic>FGM</topic><topic>Functionally gradient materials</topic><topic>Hamilton's principle</topic><topic>Honeycomb cores</topic><topic>IGA</topic><topic>Mechanical properties</topic><topic>Polynomials</topic><topic>Shear deformation</topic><topic>Shell</topic><topic>Shells</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Le, Pham Binh</creatorcontrib><creatorcontrib>Tran, Trung-Thanh</creatorcontrib><collection>ScienceDirect Open Access Titles</collection><collection>Elsevier:ScienceDirect:Open Access</collection><collection>CrossRef</collection><collection>ProQuest Central (Corporate)</collection><collection>ProQuest Central (purchase pre-March 2016)</collection><collection>Military Database (Alumni Edition)</collection><collection>ProQuest SciTech Collection</collection><collection>ProQuest Technology Collection</collection><collection>ProQuest Central (Alumni) (purchase pre-March 2016)</collection><collection>Materials Science & Engineering Collection</collection><collection>ProQuest Central (Alumni Edition)</collection><collection>ProQuest Central UK/Ireland</collection><collection>ProQuest Central Essentials</collection><collection>ProQuest Central</collection><collection>Technology Collection</collection><collection>ProQuest One Community College</collection><collection>ProQuest Central Korea</collection><collection>SciTech Premium Collection</collection><collection>ProQuest Engineering Collection</collection><collection>Military Database</collection><collection>Engineering Database</collection><collection>Access via ProQuest (Open Access)</collection><collection>ProQuest One Academic Eastern Edition (DO NOT USE)</collection><collection>ProQuest One Academic</collection><collection>ProQuest One Academic UKI Edition</collection><collection>ProQuest Central China</collection><collection>Engineering Collection</collection><collection>ProQuest Central Basic</collection><jtitle>Defence technology</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Le, Pham Binh</au><au>Tran, Trung-Thanh</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Dynamic response of honeycomb-FGS shells subjected to the dynamic loading using non-polynomial higher-order IGA</atitle><jtitle>Defence technology</jtitle><date>2024-07-01</date><risdate>2024</risdate><volume>37</volume><spage>149</spage><epage>161</epage><pages>149-161</pages><issn>2214-9147</issn><issn>2096-3459</issn><eissn>2214-9147</eissn><abstract>The main goal of this study is to use higher-order isogeometric analysis (IGA) to study the dynamic response of sandwich shells with an auxetic honeycomb core and two different functionally graded materials (FGM) skin layers (namely honeycomb-FGS shells) subjected to dynamic loading. Touratier's non-polynomial higher-order shear deformation theory (HSDT) is used due to its simplicity and performance. The governing equation is derived from Hamilton's principle. After verifying the present approach, the effect of input parameters on the dynamic response of honeycomb-FGS shells is carried out in detail.</abstract><cop>Beijing</cop><pub>Elsevier B.V</pub><doi>10.1016/j.dt.2023.12.002</doi><tpages>13</tpages><orcidid>https://orcid.org/0000-0002-1730-0590</orcidid><oa>free_for_read</oa></addata></record> |
| fulltext | fulltext |
| identifier | ISSN: 2214-9147 |
| ispartof | Defence technology, 2024-07, Vol.37, p.149-161 |
| issn | 2214-9147 2096-3459 2214-9147 |
| language | eng |
| recordid | cdi_proquest_journals_3084907487 |
| source | ProQuest One Community College; ProQuest Central (Alumni Edition); DOAJ Directory of Open Access Journals; ProQuest Central Korea; EZB-FREE-00999 freely available EZB journals; ProQuest Central UK/Ireland; Alma/SFX Local Collection; ProQuest Central |
| subjects | Auxetic honeycomb Boundary conditions Composite materials Deformation effects Dynamic loads Dynamic response Elastic foundation FGM Functionally gradient materials Hamilton's principle Honeycomb cores IGA Mechanical properties Polynomials Shear deformation Shell Shells |
| title | Dynamic response of honeycomb-FGS shells subjected to the dynamic loading using non-polynomial higher-order IGA |
| url | https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2024-12-21T13%3A40%3A47IST&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=Dynamic%20response%20of%20honeycomb-FGS%20shells%20subjected%20to%20the%20dynamic%20loading%20using%20non-polynomial%20higher-order%20IGA&rft.jtitle=Defence%20technology&rft.au=Le,%20Pham%20Binh&rft.date=2024-07-01&rft.volume=37&rft.spage=149&rft.epage=161&rft.pages=149-161&rft.issn=2214-9147&rft.eissn=2214-9147&rft_id=info:doi/10.1016/j.dt.2023.12.002&rft_dat=%3Cproquest_cross%3E3084907487%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=3084907487&rft_id=info:pmid/&rft_els_id=S2214914723003252&rfr_iscdi=true |