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Effect of load eccentricity on the buckling of thin-walled laminated C-columns
The study investigates the behaviour of short, thin-walled laminated C-columns under eccentric compression. The tested columns are simple-supported. The effect of load inaccuracy on the critical and post-critical (local buckling) states is examined. A numerical analysis by the finite element method...
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creator | Wysmulski, Pawel Teter, Andrzej Debski, Hubert |
description | The study investigates the behaviour of short, thin-walled laminated C-columns under eccentric compression. The tested columns are simple-supported. The effect of load inaccuracy on the critical and post-critical (local buckling) states is examined. A numerical analysis by the finite element method and experimental tests on a test stand are performed. The samples were produced from a carbon-epoxy prepreg by the autoclave technique. The experimental tests rest on the assumption that compressive loads are 1.5 higher than the theoretical critical force. Numerical modelling is performed using the commercial software package ABAQUS®. The critical load is determined by solving an eigen problem using the Subspace algorithm. The experimental critical loads are determined based on post-buckling paths. The numerical and experimental results show high agreement, thus demonstrating a significant effect of load inaccuracy on the critical load corresponding to the column’s local buckling. |
doi_str_mv | 10.1063/1.5019079 |
format | conference_proceeding |
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The tested columns are simple-supported. The effect of load inaccuracy on the critical and post-critical (local buckling) states is examined. A numerical analysis by the finite element method and experimental tests on a test stand are performed. The samples were produced from a carbon-epoxy prepreg by the autoclave technique. The experimental tests rest on the assumption that compressive loads are 1.5 higher than the theoretical critical force. Numerical modelling is performed using the commercial software package ABAQUS®. The critical load is determined by solving an eigen problem using the Subspace algorithm. The experimental critical loads are determined based on post-buckling paths. 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The numerical and experimental results show high agreement, thus demonstrating a significant effect of load inaccuracy on the critical load corresponding to the column’s local buckling.</description><subject>Autoclaving</subject><subject>Buckling</subject><subject>Carbon fiber reinforced plastics</subject><subject>Carbon-epoxy composites</subject><subject>Columns (structural)</subject><subject>Computer simulation</subject><subject>Finite element method</subject><subject>Load</subject><subject>Numerical analysis</subject><subject>Postbuckling</subject><subject>Test procedures</subject><issn>0094-243X</issn><issn>1551-7616</issn><fulltext>true</fulltext><rsrctype>conference_proceeding</rsrctype><creationdate>2018</creationdate><recordtype>conference_proceeding</recordtype><recordid>eNp9kM1OwzAQhC0EEqVw4A0icUNK8cZ1bB9RxZ9UwQUkbpZje2lKaofEAfXtSdVK3DjtHL6Z3R1CLoHOgJbsBmacgqJCHZEJcA65KKE8JhNK1Twv5uz9lJz1_ZrSQgkhJ-T5DtHblEXMmmhc5q31IXW1rdM2iyFLK59Vg_1s6vCxg9KqDvmPaRrvssZs6mDSqBa5jc2wCf05OUHT9P7iMKfk7f7udfGYL18enha3y7wtpEy5ZNIInANSBgorjugYM1JaNHI8vxKVQY_KAEXjBCsdRw6mpMw5L3zh2JRc7XPbLn4Nvk96HYcujCt1AcAlLRXlI3W9p_rxHZPqGHTb1RvTbfV37DToQ1e6dfgfDFTvyv0zsF-Jw2wN</recordid><startdate>20180105</startdate><enddate>20180105</enddate><creator>Wysmulski, Pawel</creator><creator>Teter, Andrzej</creator><creator>Debski, Hubert</creator><general>American Institute of Physics</general><scope>8FD</scope><scope>H8D</scope><scope>L7M</scope></search><sort><creationdate>20180105</creationdate><title>Effect of load eccentricity on the buckling of thin-walled laminated C-columns</title><author>Wysmulski, Pawel ; Teter, Andrzej ; Debski, Hubert</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-p288t-838a7f41f0319fb5ffd33a88cfa8019b7bafef9a10fad736d5f51a603dde7e2d3</frbrgroupid><rsrctype>conference_proceedings</rsrctype><prefilter>conference_proceedings</prefilter><language>eng</language><creationdate>2018</creationdate><topic>Autoclaving</topic><topic>Buckling</topic><topic>Carbon fiber reinforced plastics</topic><topic>Carbon-epoxy composites</topic><topic>Columns (structural)</topic><topic>Computer simulation</topic><topic>Finite element method</topic><topic>Load</topic><topic>Numerical analysis</topic><topic>Postbuckling</topic><topic>Test procedures</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Wysmulski, Pawel</creatorcontrib><creatorcontrib>Teter, Andrzej</creatorcontrib><creatorcontrib>Debski, Hubert</creatorcontrib><collection>Technology Research Database</collection><collection>Aerospace Database</collection><collection>Advanced Technologies Database with Aerospace</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Wysmulski, Pawel</au><au>Teter, Andrzej</au><au>Debski, Hubert</au><au>Latalski, Jarosław</au><au>Bec, Jarosław</au><au>Warminski, Jerzy</au><au>Kuczma, Mieczyslaw</au><au>Podgorski, Jerzy</au><au>Burczynski, Tadeusz</au><au>Borowa, Ewa Blazik</au><format>book</format><genre>proceeding</genre><ristype>CONF</ristype><atitle>Effect of load eccentricity on the buckling of thin-walled laminated C-columns</atitle><btitle>AIP conference proceedings</btitle><date>2018-01-05</date><risdate>2018</risdate><volume>1922</volume><issue>1</issue><issn>0094-243X</issn><eissn>1551-7616</eissn><coden>APCPCS</coden><abstract>The study investigates the behaviour of short, thin-walled laminated C-columns under eccentric compression. The tested columns are simple-supported. The effect of load inaccuracy on the critical and post-critical (local buckling) states is examined. A numerical analysis by the finite element method and experimental tests on a test stand are performed. The samples were produced from a carbon-epoxy prepreg by the autoclave technique. The experimental tests rest on the assumption that compressive loads are 1.5 higher than the theoretical critical force. Numerical modelling is performed using the commercial software package ABAQUS®. The critical load is determined by solving an eigen problem using the Subspace algorithm. The experimental critical loads are determined based on post-buckling paths. 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source | American Institute of Physics:Jisc Collections:Transitional Journals Agreement 2021-23 (Reading list) |
subjects | Autoclaving Buckling Carbon fiber reinforced plastics Carbon-epoxy composites Columns (structural) Computer simulation Finite element method Load Numerical analysis Postbuckling Test procedures |
title | Effect of load eccentricity on the buckling of thin-walled laminated C-columns |
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