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Vibration analysis for anti-symmetric laminated composite plates resting on visco-elastic foundation with temperature effects

A. Rahmani, S. Faroughi, Michael Friswell

Applied Mathematical Modelling, Volume: 94, Pages: 421 - 445

Swansea University Author: Michael Friswell

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DOI (Published version): 10.1016/j.apm.2021.01.026

Abstract

In this work, a comprehensive vibrational behavior analysis is performed on anti-symmetric laminated composite plates resting on visco-elastic foundations undergoing thermal effects. Here, the governing equations of motion are developed through Hamilton's principle and Reddy's plate theory...

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Published in: Applied Mathematical Modelling
ISSN: 0307-904X
Published: Elsevier BV 2021
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URI: https://cronfa.swan.ac.uk/Record/cronfa56190
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spelling 2025-01-15T11:34:00.2612285 v2 56190 2021-02-04 Vibration analysis for anti-symmetric laminated composite plates resting on visco-elastic foundation with temperature effects 5894777b8f9c6e64bde3568d68078d40 Michael Friswell Michael Friswell true false 2021-02-04 In this work, a comprehensive vibrational behavior analysis is performed on anti-symmetric laminated composite plates resting on visco-elastic foundations undergoing thermal effects. Here, the governing equations of motion are developed through Hamilton's principle and Reddy's plate theory as higher-order shear deformation theory (HSDT) is employed to capture high accuracy. Also, the generalized differential quadrature method (GDQM) is used to predict the vibration response and the natural frequencies. The effects of temperature change, Winkler-Pasternak and damping coefficients for the elastic foundation, the elastic ratio, the arrangement of different anti-symmetric laminates, and the aspect and slenderness ratios are observed and discussed in detail. The results are extracted for fully clamped boundary conditions and the effects of other boundary conditions are also illustrated. Journal Article Applied Mathematical Modelling 94 421 445 Elsevier BV 0307-904X Anti-symmetric Laminated Composite Plates, Thermal Effects, Elastic Foundation, Higher-Order Shear Deformation Theory, GDQM 1 6 2021 2021-06-01 10.1016/j.apm.2021.01.026 COLLEGE NANME COLLEGE CODE Swansea University Not Required 2025-01-15T11:34:00.2612285 2021-02-04T11:00:27.6678341 Faculty of Science and Engineering School of Aerospace, Civil, Electrical, General and Mechanical Engineering - Aerospace Engineering A. Rahmani 1 S. Faroughi 2 Michael Friswell 3 56190__19234__c1b6b50024aa4590bf936a48d0988e5e.pdf 56190.pdf 2021-02-04T11:04:06.8073084 Output 3979591 application/pdf Accepted Manuscript true 2022-01-29T00:00:00.0000000 ©2021 All rights reserved. All article content, except where otherwise noted, is licensed under a Creative Commons Attribution Non-Commercial No Derivatives License (CC-BY-NC-ND) true eng http://creativecommons.org/licenses/by-nc-nd/4.0/
title Vibration analysis for anti-symmetric laminated composite plates resting on visco-elastic foundation with temperature effects
spellingShingle Vibration analysis for anti-symmetric laminated composite plates resting on visco-elastic foundation with temperature effects
Michael Friswell
title_short Vibration analysis for anti-symmetric laminated composite plates resting on visco-elastic foundation with temperature effects
title_full Vibration analysis for anti-symmetric laminated composite plates resting on visco-elastic foundation with temperature effects
title_fullStr Vibration analysis for anti-symmetric laminated composite plates resting on visco-elastic foundation with temperature effects
title_full_unstemmed Vibration analysis for anti-symmetric laminated composite plates resting on visco-elastic foundation with temperature effects
title_sort Vibration analysis for anti-symmetric laminated composite plates resting on visco-elastic foundation with temperature effects
author_id_str_mv 5894777b8f9c6e64bde3568d68078d40
author_id_fullname_str_mv 5894777b8f9c6e64bde3568d68078d40_***_Michael Friswell
author Michael Friswell
author2 A. Rahmani
S. Faroughi
Michael Friswell
format Journal article
container_title Applied Mathematical Modelling
container_volume 94
container_start_page 421
publishDate 2021
institution Swansea University
issn 0307-904X
doi_str_mv 10.1016/j.apm.2021.01.026
publisher Elsevier BV
college_str Faculty of Science and Engineering
hierarchytype
hierarchy_top_id facultyofscienceandengineering
hierarchy_top_title Faculty of Science and Engineering
hierarchy_parent_id facultyofscienceandengineering
hierarchy_parent_title Faculty of Science and Engineering
department_str School of Aerospace, Civil, Electrical, General and Mechanical Engineering - Aerospace Engineering{{{_:::_}}}Faculty of Science and Engineering{{{_:::_}}}School of Aerospace, Civil, Electrical, General and Mechanical Engineering - Aerospace Engineering
document_store_str 1
active_str 0
description In this work, a comprehensive vibrational behavior analysis is performed on anti-symmetric laminated composite plates resting on visco-elastic foundations undergoing thermal effects. Here, the governing equations of motion are developed through Hamilton's principle and Reddy's plate theory as higher-order shear deformation theory (HSDT) is employed to capture high accuracy. Also, the generalized differential quadrature method (GDQM) is used to predict the vibration response and the natural frequencies. The effects of temperature change, Winkler-Pasternak and damping coefficients for the elastic foundation, the elastic ratio, the arrangement of different anti-symmetric laminates, and the aspect and slenderness ratios are observed and discussed in detail. The results are extracted for fully clamped boundary conditions and the effects of other boundary conditions are also illustrated.
published_date 2021-06-01T14:07:43Z
_version_ 1821414746583203840
score 11.543985

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