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Dynamic buckling of stiffened plates with elastically restrained edges under in-plane impact loading
The dynamic buckling of stiffened plates considering the elastically restrained edges subjected to in-plane impact loading is investigated. Navier's double Fourier series is selected as deflection function, then the large-deflection plate equations are solved by the Galerkin method and four-ord...
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Published in: | Thin-walled structures 2016-10, Vol.107, p.427-442 |
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creator | Yang, Bin Wang, De-yu |
description | The dynamic buckling of stiffened plates considering the elastically restrained edges subjected to in-plane impact loading is investigated. Navier's double Fourier series is selected as deflection function, then the large-deflection plate equations are solved by the Galerkin method and four-order Runge-kutta method is used to solve the motion equations. An instance presented in the published literature has validated the correctness of the method. The method is extended to the research of the dynamic response of the stiffened plate with elastically restrained boundary condition. The results show the rotational restraint stiffness usually ignored by previous researchers plays an important role in dynamic response of the stiffened plate under in-plane impact loading, and the influence degree of rotational restraint stiffness on dynamic buckling loads and dynamic response increase along with the initial imperfection and pulse duration. In order to accurately evaluate the dynamic buckling load, a new simple buckling criterion is presented in the paper and proven effective.
•With the increasing of R, the time of dynamic response reaches its peak decreases.•With the initial imperfections increasing, the attenuation phenomenon will be more apparent.•The influence degree of R on dynamic behaviour increases with the initial imperfections and impact duration.•Boundary conditions can be regarded as clamped when R≧20 and simply supported when R≦0.5.•A new method is used to determine the dynamic buckling load. |
doi_str_mv | 10.1016/j.tws.2016.06.019 |
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•With the increasing of R, the time of dynamic response reaches its peak decreases.•With the initial imperfections increasing, the attenuation phenomenon will be more apparent.•The influence degree of R on dynamic behaviour increases with the initial imperfections and impact duration.•Boundary conditions can be regarded as clamped when R≧20 and simply supported when R≦0.5.•A new method is used to determine the dynamic buckling load.</description><identifier>ISSN: 0263-8231</identifier><identifier>EISSN: 1879-3223</identifier><identifier>DOI: 10.1016/j.tws.2016.06.019</identifier><language>eng</language><publisher>Elsevier Ltd</publisher><subject>Buckling ; Constraints ; Dynamic buckling ; Dynamic response ; Dynamics ; Impact loading ; Initial imperfections ; Loads (forces) ; Mathematical analysis ; Plates ; Pulse duration ; Rotational restraint stiffness ; Stiffened plates</subject><ispartof>Thin-walled structures, 2016-10, Vol.107, p.427-442</ispartof><rights>2016 Elsevier Ltd</rights><lds50>peer_reviewed</lds50><woscitedreferencessubscribed>false</woscitedreferencessubscribed><citedby>FETCH-LOGICAL-c330t-e4fabe12aadf91f54b56d9ca1abc7eb23fbbd3afb1126cf95980998f3f49afdc3</citedby><cites>FETCH-LOGICAL-c330t-e4fabe12aadf91f54b56d9ca1abc7eb23fbbd3afb1126cf95980998f3f49afdc3</cites></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><link.rule.ids>314,780,784,27924,27925</link.rule.ids></links><search><creatorcontrib>Yang, Bin</creatorcontrib><creatorcontrib>Wang, De-yu</creatorcontrib><title>Dynamic buckling of stiffened plates with elastically restrained edges under in-plane impact loading</title><title>Thin-walled structures</title><description>The dynamic buckling of stiffened plates considering the elastically restrained edges subjected to in-plane impact loading is investigated. Navier's double Fourier series is selected as deflection function, then the large-deflection plate equations are solved by the Galerkin method and four-order Runge-kutta method is used to solve the motion equations. An instance presented in the published literature has validated the correctness of the method. The method is extended to the research of the dynamic response of the stiffened plate with elastically restrained boundary condition. The results show the rotational restraint stiffness usually ignored by previous researchers plays an important role in dynamic response of the stiffened plate under in-plane impact loading, and the influence degree of rotational restraint stiffness on dynamic buckling loads and dynamic response increase along with the initial imperfection and pulse duration. In order to accurately evaluate the dynamic buckling load, a new simple buckling criterion is presented in the paper and proven effective.
•With the increasing of R, the time of dynamic response reaches its peak decreases.•With the initial imperfections increasing, the attenuation phenomenon will be more apparent.•The influence degree of R on dynamic behaviour increases with the initial imperfections and impact duration.•Boundary conditions can be regarded as clamped when R≧20 and simply supported when R≦0.5.•A new method is used to determine the dynamic buckling load.</description><subject>Buckling</subject><subject>Constraints</subject><subject>Dynamic buckling</subject><subject>Dynamic response</subject><subject>Dynamics</subject><subject>Impact loading</subject><subject>Initial imperfections</subject><subject>Loads (forces)</subject><subject>Mathematical analysis</subject><subject>Plates</subject><subject>Pulse duration</subject><subject>Rotational restraint stiffness</subject><subject>Stiffened plates</subject><issn>0263-8231</issn><issn>1879-3223</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2016</creationdate><recordtype>article</recordtype><recordid>eNp9UMtOwzAQtBBIlMIHcPORS4LXTtJYnFB5SpW4wNly7HVxyaPYKVX_HkfljDTSrrQzo9kh5BpYDgyq200-7mPO05qzBJAnZAb1QmaCc3FKZoxXIqu5gHNyEeOGMViALGbEPhx63XlDm535an2_poOjcfTOYY-Wbls9YqR7P35SbHU6GN22BxowjkH7iYJ2nRi73mKgvs-Sokfqu602I20HbZPnJTlzuo149Tfn5OPp8X35kq3enl-X96vMCMHGDAunGwSutXUSXFk0ZWWl0aAbs8CGC9c0VmjXAPDKOFnKmklZO-EKqZ01Yk5ujr7bMHzvUkTV-WiwnSINu6igFmXFy1oWiQpHqglDjAGd2gbf6XBQwNTUqNqo1KiaGlUsAWTS3B01mH748RhUNB57g9YHNKOyg_9H_Qs3b4IV</recordid><startdate>201610</startdate><enddate>201610</enddate><creator>Yang, Bin</creator><creator>Wang, De-yu</creator><general>Elsevier Ltd</general><scope>AAYXX</scope><scope>CITATION</scope><scope>7SR</scope><scope>7TB</scope><scope>8BQ</scope><scope>8FD</scope><scope>FR3</scope><scope>JG9</scope><scope>KR7</scope></search><sort><creationdate>201610</creationdate><title>Dynamic buckling of stiffened plates with elastically restrained edges under in-plane impact loading</title><author>Yang, Bin ; Wang, De-yu</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-c330t-e4fabe12aadf91f54b56d9ca1abc7eb23fbbd3afb1126cf95980998f3f49afdc3</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2016</creationdate><topic>Buckling</topic><topic>Constraints</topic><topic>Dynamic buckling</topic><topic>Dynamic response</topic><topic>Dynamics</topic><topic>Impact loading</topic><topic>Initial imperfections</topic><topic>Loads (forces)</topic><topic>Mathematical analysis</topic><topic>Plates</topic><topic>Pulse duration</topic><topic>Rotational restraint stiffness</topic><topic>Stiffened plates</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Yang, Bin</creatorcontrib><creatorcontrib>Wang, De-yu</creatorcontrib><collection>CrossRef</collection><collection>Engineered Materials Abstracts</collection><collection>Mechanical & Transportation Engineering Abstracts</collection><collection>METADEX</collection><collection>Technology Research Database</collection><collection>Engineering Research Database</collection><collection>Materials Research Database</collection><collection>Civil Engineering Abstracts</collection><jtitle>Thin-walled structures</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Yang, Bin</au><au>Wang, De-yu</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Dynamic buckling of stiffened plates with elastically restrained edges under in-plane impact loading</atitle><jtitle>Thin-walled structures</jtitle><date>2016-10</date><risdate>2016</risdate><volume>107</volume><spage>427</spage><epage>442</epage><pages>427-442</pages><issn>0263-8231</issn><eissn>1879-3223</eissn><abstract>The dynamic buckling of stiffened plates considering the elastically restrained edges subjected to in-plane impact loading is investigated. Navier's double Fourier series is selected as deflection function, then the large-deflection plate equations are solved by the Galerkin method and four-order Runge-kutta method is used to solve the motion equations. An instance presented in the published literature has validated the correctness of the method. The method is extended to the research of the dynamic response of the stiffened plate with elastically restrained boundary condition. The results show the rotational restraint stiffness usually ignored by previous researchers plays an important role in dynamic response of the stiffened plate under in-plane impact loading, and the influence degree of rotational restraint stiffness on dynamic buckling loads and dynamic response increase along with the initial imperfection and pulse duration. In order to accurately evaluate the dynamic buckling load, a new simple buckling criterion is presented in the paper and proven effective.
•With the increasing of R, the time of dynamic response reaches its peak decreases.•With the initial imperfections increasing, the attenuation phenomenon will be more apparent.•The influence degree of R on dynamic behaviour increases with the initial imperfections and impact duration.•Boundary conditions can be regarded as clamped when R≧20 and simply supported when R≦0.5.•A new method is used to determine the dynamic buckling load.</abstract><pub>Elsevier Ltd</pub><doi>10.1016/j.tws.2016.06.019</doi><tpages>16</tpages></addata></record> |
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source | ScienceDirect Journals |
subjects | Buckling Constraints Dynamic buckling Dynamic response Dynamics Impact loading Initial imperfections Loads (forces) Mathematical analysis Plates Pulse duration Rotational restraint stiffness Stiffened plates |
title | Dynamic buckling of stiffened plates with elastically restrained edges under in-plane impact loading |
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