Free vibration analysis of a laminated composite beam with various boundary conditions
dc.authorid | 57192985040 | |
dc.authorid | 56303381400 | |
dc.authorid | 56304151400 | |
dc.authorid | 6602818245 | |
dc.contributor.author | Balci M. | |
dc.contributor.author | Nalbant M.O. | |
dc.contributor.author | Kara E. | |
dc.contributor.author | Gündo?du Ö | |
dc.date.accessioned | 20.04.201910:49:12 | |
dc.date.accessioned | 2019-04-20T21:44:14Z | |
dc.date.available | 20.04.201910:49:12 | |
dc.date.available | 2019-04-20T21:44:14Z | |
dc.date.issued | 2014 | |
dc.department | Bayburt Üniversitesi | en_US |
dc.description.abstract | This study presents a free vibration analysis of a laminated composite beam, based on the Euler-Bernoulli beam theory. A numerical model of the laminated composite beam was obtained for various boundary conditions based on different length-to-thickness ratios for a number of layers, using the finite element method. A planar beam bending element with two nodes, each having two degrees of freedom, was chosen according to Euler-Bernoulli beam theory. The natural frequencies of the laminated composite beam were obtained for each case, and presented in such a way as to display the effect of these changes on the natural frequencies. Eight natural frequencies of clamped-free, clamped-clamped (CC) and simple-simple (SS) composite beams were first obtained for different length-to-thickness ratios (Lx /h), numbers of layers, layer angles and for their different positions. It can be seen that natural frequencies decrease for all modes with increasing length-to-thickness ratio in all cases. © Universiti Malaysia Pahang. | en_US |
dc.identifier.doi | 10.15282/ijame.9.2013.22.0144 | |
dc.identifier.endpage | 1746 | |
dc.identifier.issn | 2229-8649 | |
dc.identifier.issue | 1 | |
dc.identifier.scopus | 2-s2.0-84905240724 | en_US |
dc.identifier.scopusquality | Q3 | en_US |
dc.identifier.startpage | 1734 | |
dc.identifier.uri | https://dx.doi.org/10.15282/ijame.9.2013.22.0144 | |
dc.identifier.uri | https://hdl.handle.net/20.500.12403/804 | |
dc.identifier.volume | 9 | |
dc.identifier.wos | WOS:000434545600021 | en_US |
dc.identifier.wosquality | N/A | en_US |
dc.indekslendigikaynak | Web of Science | en_US |
dc.indekslendigikaynak | Scopus | en_US |
dc.language.iso | en | en_US |
dc.publisher | Universiti Malaysia Pahang | |
dc.relation.ispartof | International Journal of Automotive and Mechanical Engineering | en_US |
dc.relation.publicationcategory | Makale - Uluslararası Hakemli Dergi - Kurum Öğretim Elemanı | en_US |
dc.rights | info:eu-repo/semantics/openAccess | en_US |
dc.subject | Euler-Bernoulli beam | |
dc.subject | Finite element method | |
dc.subject | Free vibration | |
dc.subject | Laminated composite beam | |
dc.subject | Euler-Bernoulli beam | |
dc.subject | Finite element method | |
dc.subject | Free vibration | |
dc.subject | Laminated composite beam | |
dc.title | Free vibration analysis of a laminated composite beam with various boundary conditions | en_US |
dc.type | Article | en_US |