BUCKLING ANALYSIS OF LAMINATED COMPOSITE PLATES USING AN EFFICIENT C0 FE MODEL

Bibliographic Details
Main Author: SINGH, SUSHIL KUMAR
Publication Date: 2012
Format: Article
Language: eng
Source: Latin American journal of solids and structures (Online)
Download full: https://www.lajss.org/index.php/LAJSS/article/view/417
Summary: BUCKLING ANALYSIS OF LAMINATED COMPOSITE PLATES IS CARRIED OUT BY USING AN EFFICIENT C0 FE MODEL DEVELOPED BASED ON HIGHER ORDER ZIGZAG THEORY. IN THIS MODEL THE FIRST DERIVATIVES OF TRANSVERSE DISPLACEMENT HAVE BEEN TREATED AS INDEPENDENT VARIABLES TO OVERCOME THE PROBLEM OF C1 CONTINUITY ASSOCIATED WITH THE FE IMPLEMENTATION OF THE PLATE THEORY. THE C0 CONTINUITY OF THE PRESENT FE MODEL IS COMPENSATED IN THE STIFFNESS MATRIX CALCULATIONS BY USING PENALTY PARAMETER APPROACH. NUMERICAL RESULTS AND COMPARISON WITH OTHER EXISTING SOLUTIONS SHOW THAT THE PRESENT MODEL IS VERY EFFICIENT IN PREDICTING THE BUCKLING RESPONSES OF LAMINATED COMPOSITES.
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network_name_str Latin American journal of solids and structures (Online)
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spelling BUCKLING ANALYSIS OF LAMINATED COMPOSITE PLATES USING AN EFFICIENT C0 FE MODELBUCKLINGLAMINATED COMPOSITESFINITE ELEMENT ANALYSISBUCKLING ANALYSIS OF LAMINATED COMPOSITE PLATES IS CARRIED OUT BY USING AN EFFICIENT C0 FE MODEL DEVELOPED BASED ON HIGHER ORDER ZIGZAG THEORY. IN THIS MODEL THE FIRST DERIVATIVES OF TRANSVERSE DISPLACEMENT HAVE BEEN TREATED AS INDEPENDENT VARIABLES TO OVERCOME THE PROBLEM OF C1 CONTINUITY ASSOCIATED WITH THE FE IMPLEMENTATION OF THE PLATE THEORY. THE C0 CONTINUITY OF THE PRESENT FE MODEL IS COMPENSATED IN THE STIFFNESS MATRIX CALCULATIONS BY USING PENALTY PARAMETER APPROACH. NUMERICAL RESULTS AND COMPARISON WITH OTHER EXISTING SOLUTIONS SHOW THAT THE PRESENT MODEL IS VERY EFFICIENT IN PREDICTING THE BUCKLING RESPONSES OF LAMINATED COMPOSITES. LAJSS is run by a team of researchers, like you!2012-06-30info:eu-repo/semantics/articleinfo:eu-repo/semantics/publishedVersionapplication/pdfhttps://www.lajss.org/index.php/LAJSS/article/view/417Latin American Journal of Solids and Structures; Vol. 9 No. 3 (2012); 3531679-78251679-7817reponame:Latin American journal of solids and structures (Online)instname:Associação Brasileira de Engenharia e Ciências Mecânicas (ABCM)instacron:ABCMenghttps://www.lajss.org/index.php/LAJSS/article/view/417/378Copyright (c) 2018 LATIN AMERICAN JOURNAL OF SOLIDS AND STRUCTURESinfo:eu-repo/semantics/openAccessSINGH, SUSHIL KUMAR2012-07-11T15:29:05Zoai:ojs.pkp.sfu.ca:article/417Revistahttps://www.lajss.org/index.php/LAJSS/PRIhttps://www.lajss.org/index.php/LAJSS/oaiabcm@abcm.org.br||maralves@usp.br||lajsssecretary@gmsie.usp.br1679-78251679-7817opendoar:2012-07-11T15:29:05Latin American journal of solids and structures (Online) - Associação Brasileira de Engenharia e Ciências Mecânicas (ABCM)false
dc.title.none.fl_str_mv BUCKLING ANALYSIS OF LAMINATED COMPOSITE PLATES USING AN EFFICIENT C0 FE MODEL
title BUCKLING ANALYSIS OF LAMINATED COMPOSITE PLATES USING AN EFFICIENT C0 FE MODEL
spellingShingle BUCKLING ANALYSIS OF LAMINATED COMPOSITE PLATES USING AN EFFICIENT C0 FE MODEL
SINGH, SUSHIL KUMAR
BUCKLING
LAMINATED COMPOSITES
FINITE ELEMENT ANALYSIS
title_short BUCKLING ANALYSIS OF LAMINATED COMPOSITE PLATES USING AN EFFICIENT C0 FE MODEL
title_full BUCKLING ANALYSIS OF LAMINATED COMPOSITE PLATES USING AN EFFICIENT C0 FE MODEL
title_fullStr BUCKLING ANALYSIS OF LAMINATED COMPOSITE PLATES USING AN EFFICIENT C0 FE MODEL
title_full_unstemmed BUCKLING ANALYSIS OF LAMINATED COMPOSITE PLATES USING AN EFFICIENT C0 FE MODEL
title_sort BUCKLING ANALYSIS OF LAMINATED COMPOSITE PLATES USING AN EFFICIENT C0 FE MODEL
author SINGH, SUSHIL KUMAR
author_facet SINGH, SUSHIL KUMAR
author_role author
dc.contributor.author.fl_str_mv SINGH, SUSHIL KUMAR
dc.subject.por.fl_str_mv BUCKLING
LAMINATED COMPOSITES
FINITE ELEMENT ANALYSIS
topic BUCKLING
LAMINATED COMPOSITES
FINITE ELEMENT ANALYSIS
description BUCKLING ANALYSIS OF LAMINATED COMPOSITE PLATES IS CARRIED OUT BY USING AN EFFICIENT C0 FE MODEL DEVELOPED BASED ON HIGHER ORDER ZIGZAG THEORY. IN THIS MODEL THE FIRST DERIVATIVES OF TRANSVERSE DISPLACEMENT HAVE BEEN TREATED AS INDEPENDENT VARIABLES TO OVERCOME THE PROBLEM OF C1 CONTINUITY ASSOCIATED WITH THE FE IMPLEMENTATION OF THE PLATE THEORY. THE C0 CONTINUITY OF THE PRESENT FE MODEL IS COMPENSATED IN THE STIFFNESS MATRIX CALCULATIONS BY USING PENALTY PARAMETER APPROACH. NUMERICAL RESULTS AND COMPARISON WITH OTHER EXISTING SOLUTIONS SHOW THAT THE PRESENT MODEL IS VERY EFFICIENT IN PREDICTING THE BUCKLING RESPONSES OF LAMINATED COMPOSITES.
publishDate 2012
dc.date.none.fl_str_mv 2012-06-30
dc.type.driver.fl_str_mv info:eu-repo/semantics/article
info:eu-repo/semantics/publishedVersion
format article
status_str publishedVersion
dc.identifier.uri.fl_str_mv https://www.lajss.org/index.php/LAJSS/article/view/417
url https://www.lajss.org/index.php/LAJSS/article/view/417
dc.language.iso.fl_str_mv eng
language eng
dc.relation.none.fl_str_mv https://www.lajss.org/index.php/LAJSS/article/view/417/378
dc.rights.driver.fl_str_mv Copyright (c) 2018 LATIN AMERICAN JOURNAL OF SOLIDS AND STRUCTURES
info:eu-repo/semantics/openAccess
rights_invalid_str_mv Copyright (c) 2018 LATIN AMERICAN JOURNAL OF SOLIDS AND STRUCTURES
eu_rights_str_mv openAccess
dc.format.none.fl_str_mv application/pdf
dc.publisher.none.fl_str_mv LAJSS is run by a team of researchers, like you!
publisher.none.fl_str_mv LAJSS is run by a team of researchers, like you!
dc.source.none.fl_str_mv Latin American Journal of Solids and Structures; Vol. 9 No. 3 (2012); 353
1679-7825
1679-7817
reponame:Latin American journal of solids and structures (Online)
instname:Associação Brasileira de Engenharia e Ciências Mecânicas (ABCM)
instacron:ABCM
instname_str Associação Brasileira de Engenharia e Ciências Mecânicas (ABCM)
instacron_str ABCM
institution ABCM
reponame_str Latin American journal of solids and structures (Online)
collection Latin American journal of solids and structures (Online)
repository.name.fl_str_mv Latin American journal of solids and structures (Online) - Associação Brasileira de Engenharia e Ciências Mecânicas (ABCM)
repository.mail.fl_str_mv abcm@abcm.org.br||maralves@usp.br||lajsssecretary@gmsie.usp.br
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