Isogeometric Dynamic Buckling Analysis of Trimmed and Multipatch Thin-Shell Structures
This paper extends our previous work on the isogeometric dynamic buckling analysis of thin-shell structures to the trimmed and multipatch situation where features such as cutouts and stiffeners can be easily incorporated. To be specific, a modified generalized-α time integration scheme combined with...
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Veröffentlicht in: | AIAA journal 2023-12, Vol.61 (12), p.5620-5634 |
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description | This paper extends our previous work on the isogeometric dynamic buckling analysis of thin-shell structures to the trimmed and multipatch situation where features such as cutouts and stiffeners can be easily incorporated. To be specific, a modified generalized-α time integration scheme combined with a geometric nonlinear isogeometric Kirchhoff–Love shell element is used to simulate the complex buckling and postbuckling behaviors of thin-shell structures. The developed method can damp properly high-frequency contents while maintaining second-order accuracy in the dynamic buckling analysis. For the integration of arbitrary-shaped trimmed elements, a geometrically exact blending function method is developed to improve the efficiency of the dynamic shell buckling analysis. To deal with multipatch geometries, a penalty-based weak coupling approach is developed, where coupled patches with nonconforming trimmed interfaces or even with prescribed angles, such as stiffeners, can be analyzed. We demonstrate the accuracy, stability, and flexibility of the proposed framework with several numerical examples. In particular, the influences of “free” and “partially free” control points, penalty factor, trimming, as well as different modeling strategies on the dynamic solutions of shell structures are investigated. |
doi_str_mv | 10.2514/1.J063273 |
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To be specific, a modified generalized-α time integration scheme combined with a geometric nonlinear isogeometric Kirchhoff–Love shell element is used to simulate the complex buckling and postbuckling behaviors of thin-shell structures. The developed method can damp properly high-frequency contents while maintaining second-order accuracy in the dynamic buckling analysis. For the integration of arbitrary-shaped trimmed elements, a geometrically exact blending function method is developed to improve the efficiency of the dynamic shell buckling analysis. To deal with multipatch geometries, a penalty-based weak coupling approach is developed, where coupled patches with nonconforming trimmed interfaces or even with prescribed angles, such as stiffeners, can be analyzed. We demonstrate the accuracy, stability, and flexibility of the proposed framework with several numerical examples. In particular, the influences of “free” and “partially free” control points, penalty factor, trimming, as well as different modeling strategies on the dynamic solutions of shell structures are investigated.</description><identifier>ISSN: 0001-1452</identifier><identifier>EISSN: 1533-385X</identifier><identifier>DOI: 10.2514/1.J063273</identifier><language>eng</language><publisher>Virginia: American Institute of Aeronautics and Astronautics</publisher><subject>Accuracy ; Aeronautics ; Aerospace engineering ; Angles (geometry) ; Approximation ; Methods ; Postbuckling ; Shells (structural forms) ; Stability analysis ; Stiffeners ; Time integration</subject><ispartof>AIAA journal, 2023-12, Vol.61 (12), p.5620-5634</ispartof><rights>Copyright © 2023 by the American Institute of Aeronautics and Astronautics, Inc. All rights reserved. All requests for copying and permission to reprint should be submitted to CCC at ; employ the eISSN to initiate your request. See also AIAA Rights and Permissions .</rights><rights>Copyright © 2023 by the American Institute of Aeronautics and Astronautics, Inc. All rights reserved. All requests for copying and permission to reprint should be submitted to CCC at www.copyright.com; employ the eISSN 1533-385X to initiate your request. See also AIAA Rights and Permissions www.aiaa.org/randp.</rights><lds50>peer_reviewed</lds50><woscitedreferencessubscribed>false</woscitedreferencessubscribed><cites>FETCH-LOGICAL-a248t-19a0cb4d88860e3ebc97a8b52438c16039937378471c050d05a7e4fb65ed00293</cites><orcidid>0000-0001-7160-4838 ; 0000-0001-7252-2367</orcidid></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><link.rule.ids>314,776,780,27901,27902</link.rule.ids></links><search><creatorcontrib>Guo, Yujie</creatorcontrib><creatorcontrib>Chen, Zhaolin</creatorcontrib><creatorcontrib>Wei, Xiaohui</creatorcontrib><creatorcontrib>Hong, Zhi</creatorcontrib><title>Isogeometric Dynamic Buckling Analysis of Trimmed and Multipatch Thin-Shell Structures</title><title>AIAA journal</title><description>This paper extends our previous work on the isogeometric dynamic buckling analysis of thin-shell structures to the trimmed and multipatch situation where features such as cutouts and stiffeners can be easily incorporated. To be specific, a modified generalized-α time integration scheme combined with a geometric nonlinear isogeometric Kirchhoff–Love shell element is used to simulate the complex buckling and postbuckling behaviors of thin-shell structures. The developed method can damp properly high-frequency contents while maintaining second-order accuracy in the dynamic buckling analysis. For the integration of arbitrary-shaped trimmed elements, a geometrically exact blending function method is developed to improve the efficiency of the dynamic shell buckling analysis. To deal with multipatch geometries, a penalty-based weak coupling approach is developed, where coupled patches with nonconforming trimmed interfaces or even with prescribed angles, such as stiffeners, can be analyzed. We demonstrate the accuracy, stability, and flexibility of the proposed framework with several numerical examples. In particular, the influences of “free” and “partially free” control points, penalty factor, trimming, as well as different modeling strategies on the dynamic solutions of shell structures are investigated.</description><subject>Accuracy</subject><subject>Aeronautics</subject><subject>Aerospace engineering</subject><subject>Angles (geometry)</subject><subject>Approximation</subject><subject>Methods</subject><subject>Postbuckling</subject><subject>Shells (structural forms)</subject><subject>Stability analysis</subject><subject>Stiffeners</subject><subject>Time integration</subject><issn>0001-1452</issn><issn>1533-385X</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2023</creationdate><recordtype>article</recordtype><recordid>eNplkEtLAzEAhIMoWKsH_0FAEDxszXOTHGt9VSoeWsVbyGaz7dZ91CR72H_vSgsePA0DH8PMAHCJ0YRwzG7x5AWllAh6BEaYU5pQyT-PwQghhBPMODkFZyFsB0eExCPwMQ_t2rW1i7608L5vTD3oXWe_qrJZw2ljqj6UAbYFXPmyrl0OTZPD166K5c5Eu4GrTdkky42rKriMvrOx8y6cg5PCVMFdHHQM3h8fVrPnZPH2NJ9NF4khTMYEK4NsxnIpZYocdZlVwsiME0alxSmiSlFBhWQCW8RRjrgRjhVZyl2OEFF0DK72uTvffncuRL1tOz-UDppIJYhiQpGButlT1rcheFfo3bDF-F5jpH9v01gfbhvY6z1rSmP-0v6DP0ybaeg</recordid><startdate>20231201</startdate><enddate>20231201</enddate><creator>Guo, Yujie</creator><creator>Chen, Zhaolin</creator><creator>Wei, Xiaohui</creator><creator>Hong, Zhi</creator><general>American Institute of Aeronautics and Astronautics</general><scope>AAYXX</scope><scope>CITATION</scope><scope>7TB</scope><scope>8FD</scope><scope>FR3</scope><scope>H8D</scope><scope>L7M</scope><orcidid>https://orcid.org/0000-0001-7160-4838</orcidid><orcidid>https://orcid.org/0000-0001-7252-2367</orcidid></search><sort><creationdate>20231201</creationdate><title>Isogeometric Dynamic Buckling Analysis of Trimmed and Multipatch Thin-Shell Structures</title><author>Guo, Yujie ; Chen, Zhaolin ; Wei, Xiaohui ; Hong, Zhi</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-a248t-19a0cb4d88860e3ebc97a8b52438c16039937378471c050d05a7e4fb65ed00293</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2023</creationdate><topic>Accuracy</topic><topic>Aeronautics</topic><topic>Aerospace engineering</topic><topic>Angles (geometry)</topic><topic>Approximation</topic><topic>Methods</topic><topic>Postbuckling</topic><topic>Shells (structural forms)</topic><topic>Stability analysis</topic><topic>Stiffeners</topic><topic>Time integration</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Guo, Yujie</creatorcontrib><creatorcontrib>Chen, Zhaolin</creatorcontrib><creatorcontrib>Wei, Xiaohui</creatorcontrib><creatorcontrib>Hong, Zhi</creatorcontrib><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><jtitle>AIAA journal</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Guo, Yujie</au><au>Chen, Zhaolin</au><au>Wei, Xiaohui</au><au>Hong, Zhi</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Isogeometric Dynamic Buckling Analysis of Trimmed and Multipatch Thin-Shell Structures</atitle><jtitle>AIAA journal</jtitle><date>2023-12-01</date><risdate>2023</risdate><volume>61</volume><issue>12</issue><spage>5620</spage><epage>5634</epage><pages>5620-5634</pages><issn>0001-1452</issn><eissn>1533-385X</eissn><abstract>This paper extends our previous work on the isogeometric dynamic buckling analysis of thin-shell structures to the trimmed and multipatch situation where features such as cutouts and stiffeners can be easily incorporated. To be specific, a modified generalized-α time integration scheme combined with a geometric nonlinear isogeometric Kirchhoff–Love shell element is used to simulate the complex buckling and postbuckling behaviors of thin-shell structures. The developed method can damp properly high-frequency contents while maintaining second-order accuracy in the dynamic buckling analysis. For the integration of arbitrary-shaped trimmed elements, a geometrically exact blending function method is developed to improve the efficiency of the dynamic shell buckling analysis. To deal with multipatch geometries, a penalty-based weak coupling approach is developed, where coupled patches with nonconforming trimmed interfaces or even with prescribed angles, such as stiffeners, can be analyzed. We demonstrate the accuracy, stability, and flexibility of the proposed framework with several numerical examples. 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subjects | Accuracy Aeronautics Aerospace engineering Angles (geometry) Approximation Methods Postbuckling Shells (structural forms) Stability analysis Stiffeners Time integration |
title | Isogeometric Dynamic Buckling Analysis of Trimmed and Multipatch Thin-Shell Structures |
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