Dynamic Analysis of Linear Viscoelastic Cylindrical and Conical Helicoidal Rods Using the Mixed Fem

dc.contributor.author Eratli, Nihal
dc.contributor.author Argeso, Hakan
dc.contributor.author Calim, Faruk F.
dc.contributor.author Temel, Beytullah
dc.contributor.author Omurtag, Mehmet H.
dc.contributor.other Manufacturing Engineering
dc.date.accessioned 2024-07-05T14:26:45Z
dc.date.available 2024-07-05T14:26:45Z
dc.date.issued 2014
dc.description Eratlı, Nihal/0000-0003-3788-9870; OMURTAG, Mehmet Hakki/0000-0003-2669-6459 en_US
dc.description.abstract The objective of this study is to investigate the influence of the rotary inertia on dynamic behavior of linear viscoelastic cylindrical and conical helixes by means of the Laplace transform-mixed finite element formulation and solution. The element matrix is based on the Timoshenko beam theory. The influence of rotary inertias is considered in the dynamic analysis, which is original in the literature. Rectangular, sine and step type of impulsive loads are applied on helices having rectangular cross-sections with various aspect ratios. The Kelvin and standard models are used for defining the linear viscoelastic material behavior; and by means of the correspondence principle (the elastic-viscoelastic analogy), the material parameters are replaced with their complex counterparts in the Laplace domain. The analysis is carried out in the Laplace domain and the results are transformed back to time space numerically by modified Durbin's algorithm. First, the solution algorithm is verified using the existing open sources in the literature and afterwards some benchmark examples such as conical viscoelastic rods are handled. (C) 2014 Elsevier Ltd. All rights reserved. en_US
dc.description.sponsorship Scientific and Technological Research Council of Turkey [111M308]; Research Foundation of ITU [36130] en_US
dc.description.sponsorship This research is supported by the Scientific and Technological Research Council of Turkey under Project no. 111M308 and by the Research Foundation of ITU under Project no. 36130. These supports are gratefully acknowledged by the authors. en_US
dc.identifier.doi 10.1016/j.jsv.2014.03.017
dc.identifier.issn 0022-460X
dc.identifier.issn 1095-8568
dc.identifier.scopus 2-s2.0-84904132988
dc.identifier.uri https://doi.org/10.1016/j.jsv.2014.03.017
dc.identifier.uri https://hdl.handle.net/20.500.14411/156
dc.language.iso en en_US
dc.publisher Academic Press Ltd- Elsevier Science Ltd en_US
dc.rights info:eu-repo/semantics/closedAccess en_US
dc.subject [No Keyword Available] en_US
dc.title Dynamic Analysis of Linear Viscoelastic Cylindrical and Conical Helicoidal Rods Using the Mixed Fem en_US
dc.type Article en_US
dspace.entity.type Publication
gdc.author.id Eratlı, Nihal/0000-0003-3788-9870
gdc.author.id OMURTAG, Mehmet Hakki/0000-0003-2669-6459
gdc.author.institutional Argeşo, Ahmet Hakan
gdc.author.scopusid 6506849928
gdc.author.scopusid 8213483900
gdc.author.scopusid 8392630900
gdc.author.scopusid 6603496934
gdc.author.scopusid 6602741488
gdc.author.wosid Eratlı, Nihal/J-4845-2014
gdc.author.wosid TEMEL, Beytullah/J-1940-2018
gdc.author.wosid Omurtag, Mehmet/M-4536-2013
gdc.author.wosid CALIM, FARUK FIRAT/AAJ-7752-2021
gdc.coar.access metadata only access
gdc.coar.type text::journal::journal article
gdc.description.department Atılım University en_US
gdc.description.departmenttemp [Eratli, Nihal; Omurtag, Mehmet H.] Tech Univ Istanbul, Dept Civil Engn, Istanbul, Turkey; [Argeso, Hakan] Atilim Univ, Dept Mfg Engn, Ankara, Turkey; [Calim, Faruk F.] Mustafa Kemal Univ, Dept Civil Engn, Iskenderun, Hatay, Turkey; [Temel, Beytullah] Cukurova Univ, Dept Civil Engn, Adana, Turkey en_US
gdc.description.endpage 3690 en_US
gdc.description.issue 16 en_US
gdc.description.publicationcategory Makale - Uluslararası Hakemli Dergi - Kurum Öğretim Elemanı en_US
gdc.description.scopusquality Q1
gdc.description.startpage 3671 en_US
gdc.description.volume 333 en_US
gdc.description.wosquality Q1
gdc.identifier.wos WOS:000336822300007
gdc.scopus.citedcount 35
gdc.wos.citedcount 35
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