FRACTURE OF LAMINATED RECTANGULAR BAR AFTER BUCKLING
The delamination of composite constructional elements is determined by normal stresses and shear stresses. The non-linear strength criterion is suggested by the authors in case of complex state of stress. Fracture of laminate bar after buckling is described by mixed fracture spreading regularities....
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Veröffentlicht in: | Mechanika (Kaunas, Lithuania : 1995) Lithuania : 1995), 2011-01, Vol.17 (4), p.352-357 |
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container_title | Mechanika (Kaunas, Lithuania : 1995) |
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creator | Ziliukas, A. Malatokiene, A. |
description | The delamination of composite constructional elements is determined by normal stresses and shear stresses. The non-linear strength criterion is suggested by the authors in case of complex state of stress. Fracture of laminate bar after buckling is described by mixed fracture spreading regularities. Dependence of fracture energy on mechanical characteristics of the layers and shear resistance of the interlayer is presented. The obtained theoretical values are based on experimental investigation of glass plastic. |
doi_str_mv | 10.5755/j01.mech.17.4.560 |
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The non-linear strength criterion is suggested by the authors in case of complex state of stress. Fracture of laminate bar after buckling is described by mixed fracture spreading regularities. Dependence of fracture energy on mechanical characteristics of the layers and shear resistance of the interlayer is presented. 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The obtained theoretical values are based on experimental investigation of glass plastic.</description><subject>Buckling</subject><subject>Fracture mechanics</subject><subject>Interlayers</subject><subject>Laminates</subject><subject>Regularity</subject><subject>Shear stress</subject><subject>Spreading</subject><subject>Stresses</subject><issn>1392-1207</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2011</creationdate><recordtype>article</recordtype><recordid>eNotkL1ugzAYRT20UtO0D9CNrRP08x-2R5dCikqJhGC2XDBqIigpToa-fYjS4ere4egOB6EnDBEXnL_sAUeja78jLCIW8Rhu0ApTRUJMQNyhe-_3AJwTiVeIZZVO6qZKg20WFPozL3WdvgVVmtS63DSFroLXJTqr02U1yUeRl5sHdNvbwbvH_16jJkvr5D0stps80UXYEiGOYay-wPYs7hmxHSGd47SDviWc8045KrikDFNHQdkOCFNSKoiVkj2zrYMO6Bo9X38P8_R7cv5oxp1v3TDYHzedvFExlVwSJRcSX8l2nryfXW8O826085_BYC5SzCLFXKQYLAwzixR6Bkv9UfI</recordid><startdate>20110101</startdate><enddate>20110101</enddate><creator>Ziliukas, A.</creator><creator>Malatokiene, A.</creator><scope>AAYXX</scope><scope>CITATION</scope><scope>7TB</scope><scope>8FD</scope><scope>FR3</scope><scope>KR7</scope></search><sort><creationdate>20110101</creationdate><title>FRACTURE OF LAMINATED RECTANGULAR BAR AFTER BUCKLING</title><author>Ziliukas, A. ; Malatokiene, A.</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-c277t-69b0af46f42ad22de53d0fc2555d9e37583413e309ad024988906998f4ace0d03</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2011</creationdate><topic>Buckling</topic><topic>Fracture mechanics</topic><topic>Interlayers</topic><topic>Laminates</topic><topic>Regularity</topic><topic>Shear stress</topic><topic>Spreading</topic><topic>Stresses</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Ziliukas, A.</creatorcontrib><creatorcontrib>Malatokiene, A.</creatorcontrib><collection>CrossRef</collection><collection>Mechanical & Transportation Engineering Abstracts</collection><collection>Technology Research Database</collection><collection>Engineering Research Database</collection><collection>Civil Engineering Abstracts</collection><jtitle>Mechanika (Kaunas, Lithuania : 1995)</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Ziliukas, A.</au><au>Malatokiene, A.</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>FRACTURE OF LAMINATED RECTANGULAR BAR AFTER BUCKLING</atitle><jtitle>Mechanika (Kaunas, Lithuania : 1995)</jtitle><date>2011-01-01</date><risdate>2011</risdate><volume>17</volume><issue>4</issue><spage>352</spage><epage>357</epage><pages>352-357</pages><issn>1392-1207</issn><abstract>The delamination of composite constructional elements is determined by normal stresses and shear stresses. The non-linear strength criterion is suggested by the authors in case of complex state of stress. Fracture of laminate bar after buckling is described by mixed fracture spreading regularities. Dependence of fracture energy on mechanical characteristics of the layers and shear resistance of the interlayer is presented. The obtained theoretical values are based on experimental investigation of glass plastic.</abstract><doi>10.5755/j01.mech.17.4.560</doi><tpages>6</tpages></addata></record> |
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ispartof | Mechanika (Kaunas, Lithuania : 1995), 2011-01, Vol.17 (4), p.352-357 |
issn | 1392-1207 |
language | eng |
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source | DOAJ Directory of Open Access Journals |
subjects | Buckling Fracture mechanics Interlayers Laminates Regularity Shear stress Spreading Stresses |
title | FRACTURE OF LAMINATED RECTANGULAR BAR AFTER BUCKLING |
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