Vibration analysis of size dependent micro FML cylindrical shell reinforced by CNTs based on modified couple stress theory

In this manuscript, the sequel of agglomeration on the vibration of fiber metal laminated (FML) cylindrical shell in the micro phase using developed couple stress theory (MCST). Hamilton’s principle has been carried out for deriving the non-classical equations of motion of size dependent thin micro...

詳細記述

保存先:
書誌詳細
主要な著者: Gang Zhao, Mostafa Hooman, Mahdireza Yarigarravesh, Mohammed Algarni, Maria Jade Catalan Opulencia, Fahad Alsaikhan, Abduladheem Turki Jalil, Abdullah Mohamed, Kareem M.AboRas, Md. Lutfor Rahman, Mohd Sani Sarjadi
フォーマット: 論文
言語:English
English
出版事項: King Saud University 2022
主題:
オンライン・アクセス:https://eprints.ums.edu.my/id/eprint/34211/1/Vibration%20analysis%20of%20size%20dependent%20micro%20FML%20cylindrical%20shell%20reinforced%20by%20CNTs%20based%20on%20modified%20couple%20stress%20theory.pdf
https://eprints.ums.edu.my/id/eprint/34211/2/Vibration%20analysis%20of%20size%20dependent%20micro%20FML%20cylindrical%20shell%20reinforced%20by%20CNTs%20based%20on%20modified%20couple%20stress%20theory1.pdf
https://eprints.ums.edu.my/id/eprint/34211/
https://www.sciencedirect.com/science/article/pii/S1878535222004312
https://doi.org/10.1016/j.arabjc.2022.104115
タグ: タグ追加
タグなし, このレコードへの初めてのタグを付けませんか!
id my.ums.eprints.34211
record_format eprints
spelling my.ums.eprints.342112022-09-26T00:44:25Z https://eprints.ums.edu.my/id/eprint/34211/ Vibration analysis of size dependent micro FML cylindrical shell reinforced by CNTs based on modified couple stress theory Gang Zhao Mostafa Hooman Mahdireza Yarigarravesh Mohammed Algarni Maria Jade Catalan Opulencia Fahad Alsaikhan Abduladheem Turki Jalil Abdullah Mohamed Kareem M.AboRas Md. Lutfor Rahman Mohd Sani Sarjadi Q1-390 Science (General) In this manuscript, the sequel of agglomeration on the vibration of fiber metal laminated (FML) cylindrical shell in the micro phase using developed couple stress theory (MCST). Hamilton’s principle has been carried out for deriving the non-classical equations of motion of size dependent thin micro cylindrical shell on the basis of Love’s first approximation theory. Mori Tanaka and extended rule of mixture are utilized to estimate the mechanical attributes of carbon nanotubes (CNTs) and equivalent fiber, respectively. These four phases CNTs/fiber/polymer/metal laminated (CNTFPML) micro cylindrical shell is analyzed applying beam modal function model for several boundary limitations. Then, an investigation is performed to study the impacts of differing input parameters namely material length scale parameter, agglomeration, the distributions of agglomerated CNTs, the mass fraction of equivalent fiber and the volume fraction of CNTs on the frequency response of micro agglomerated CNTFPML cylindrical shell. The main output illustrated that the growth of frequencies is directly dependent to the increase of material length scale parameter for this agglomerated CNTFPML cylindrical shell so that through increasing the values of agglomeration parameters g and l and material length scale parameter l altogether, the frequencies of this cylindrical shell grow King Saud University 2022 Article PeerReviewed text en https://eprints.ums.edu.my/id/eprint/34211/1/Vibration%20analysis%20of%20size%20dependent%20micro%20FML%20cylindrical%20shell%20reinforced%20by%20CNTs%20based%20on%20modified%20couple%20stress%20theory.pdf text en https://eprints.ums.edu.my/id/eprint/34211/2/Vibration%20analysis%20of%20size%20dependent%20micro%20FML%20cylindrical%20shell%20reinforced%20by%20CNTs%20based%20on%20modified%20couple%20stress%20theory1.pdf Gang Zhao and Mostafa Hooman and Mahdireza Yarigarravesh and Mohammed Algarni and Maria Jade Catalan Opulencia and Fahad Alsaikhan and Abduladheem Turki Jalil and Abdullah Mohamed and Kareem M.AboRas and Md. Lutfor Rahman and Mohd Sani Sarjadi (2022) Vibration analysis of size dependent micro FML cylindrical shell reinforced by CNTs based on modified couple stress theory. Arabian Journal of Chemistry, 15. pp. 1-18. ISSN 1878-5352 https://www.sciencedirect.com/science/article/pii/S1878535222004312 https://doi.org/10.1016/j.arabjc.2022.104115
institution Universiti Malaysia Sabah
building UMS Library
collection Institutional Repository
continent Asia
country Malaysia
content_provider Universiti Malaysia Sabah
content_source UMS Institutional Repository
url_provider http://eprints.ums.edu.my/
language English
English
topic Q1-390 Science (General)
spellingShingle Q1-390 Science (General)
Gang Zhao
Mostafa Hooman
Mahdireza Yarigarravesh
Mohammed Algarni
Maria Jade Catalan Opulencia
Fahad Alsaikhan
Abduladheem Turki Jalil
Abdullah Mohamed
Kareem M.AboRas
Md. Lutfor Rahman
Mohd Sani Sarjadi
Vibration analysis of size dependent micro FML cylindrical shell reinforced by CNTs based on modified couple stress theory
description In this manuscript, the sequel of agglomeration on the vibration of fiber metal laminated (FML) cylindrical shell in the micro phase using developed couple stress theory (MCST). Hamilton’s principle has been carried out for deriving the non-classical equations of motion of size dependent thin micro cylindrical shell on the basis of Love’s first approximation theory. Mori Tanaka and extended rule of mixture are utilized to estimate the mechanical attributes of carbon nanotubes (CNTs) and equivalent fiber, respectively. These four phases CNTs/fiber/polymer/metal laminated (CNTFPML) micro cylindrical shell is analyzed applying beam modal function model for several boundary limitations. Then, an investigation is performed to study the impacts of differing input parameters namely material length scale parameter, agglomeration, the distributions of agglomerated CNTs, the mass fraction of equivalent fiber and the volume fraction of CNTs on the frequency response of micro agglomerated CNTFPML cylindrical shell. The main output illustrated that the growth of frequencies is directly dependent to the increase of material length scale parameter for this agglomerated CNTFPML cylindrical shell so that through increasing the values of agglomeration parameters g and l and material length scale parameter l altogether, the frequencies of this cylindrical shell grow
format Article
author Gang Zhao
Mostafa Hooman
Mahdireza Yarigarravesh
Mohammed Algarni
Maria Jade Catalan Opulencia
Fahad Alsaikhan
Abduladheem Turki Jalil
Abdullah Mohamed
Kareem M.AboRas
Md. Lutfor Rahman
Mohd Sani Sarjadi
author_facet Gang Zhao
Mostafa Hooman
Mahdireza Yarigarravesh
Mohammed Algarni
Maria Jade Catalan Opulencia
Fahad Alsaikhan
Abduladheem Turki Jalil
Abdullah Mohamed
Kareem M.AboRas
Md. Lutfor Rahman
Mohd Sani Sarjadi
author_sort Gang Zhao
title Vibration analysis of size dependent micro FML cylindrical shell reinforced by CNTs based on modified couple stress theory
title_short Vibration analysis of size dependent micro FML cylindrical shell reinforced by CNTs based on modified couple stress theory
title_full Vibration analysis of size dependent micro FML cylindrical shell reinforced by CNTs based on modified couple stress theory
title_fullStr Vibration analysis of size dependent micro FML cylindrical shell reinforced by CNTs based on modified couple stress theory
title_full_unstemmed Vibration analysis of size dependent micro FML cylindrical shell reinforced by CNTs based on modified couple stress theory
title_sort vibration analysis of size dependent micro fml cylindrical shell reinforced by cnts based on modified couple stress theory
publisher King Saud University
publishDate 2022
url https://eprints.ums.edu.my/id/eprint/34211/1/Vibration%20analysis%20of%20size%20dependent%20micro%20FML%20cylindrical%20shell%20reinforced%20by%20CNTs%20based%20on%20modified%20couple%20stress%20theory.pdf
https://eprints.ums.edu.my/id/eprint/34211/2/Vibration%20analysis%20of%20size%20dependent%20micro%20FML%20cylindrical%20shell%20reinforced%20by%20CNTs%20based%20on%20modified%20couple%20stress%20theory1.pdf
https://eprints.ums.edu.my/id/eprint/34211/
https://www.sciencedirect.com/science/article/pii/S1878535222004312
https://doi.org/10.1016/j.arabjc.2022.104115
_version_ 1760231264884883456
score 13.251813