Moving load analysis on cross/angle-ply laminated composite nanoplates resting on viscoelastic foundation
In this research contribution, size-dependent forced vibration analysis of embedded cross/angle-plies laminated composite nanoplate in a viscoelastic foundation while subjected to a moving load is investigated. Through Hamiltonian principle, the governing motion equations are derived on the basis of...
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Elsevier Ltd
2023
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2-s2.0-85143543828 Hai T.; Al-Masoudy M.M.; Alsulamy S.; Hechmi El Ouni M.; Ayvazyan A.; Kumar A. Moving load analysis on cross/angle-ply laminated composite nanoplates resting on viscoelastic foundation 2023 Composite Structures 305 10.1016/j.compstruct.2022.116540 https://www.scopus.com/inward/record.uri?eid=2-s2.0-85143543828&doi=10.1016%2fj.compstruct.2022.116540&partnerID=40&md5=5f9cd26936d9f686526021206b82ed08 In this research contribution, size-dependent forced vibration analysis of embedded cross/angle-plies laminated composite nanoplate in a viscoelastic foundation while subjected to a moving load is investigated. Through Hamiltonian principle, the governing motion equations are derived on the basis of a four-variable refined higher-order shear deformation theory (RHSDT) in Cartesian coordinate and Eringen nonlocal differential model (ENDM) is used in order to predict the size-dependent effects. Afterwards, in order to solve the equations, a time-dependent system of state-space in conjunction with an analytical solution method is implemented over the structures. For the first time, the effect of lay-up numbers and sequences, fiber orientations of involved layers, elastic/viscoelastic foundation coefficients, and nanoplate geometries on the size-dependent dynamic response of laminated composite nanoplate under moving concentrated load with different values of velocity and time history is examined. © 2022 Elsevier Ltd Elsevier Ltd 02638223 English Article |
author |
Hai T.; Al-Masoudy M.M.; Alsulamy S.; Hechmi El Ouni M.; Ayvazyan A.; Kumar A. |
spellingShingle |
Hai T.; Al-Masoudy M.M.; Alsulamy S.; Hechmi El Ouni M.; Ayvazyan A.; Kumar A. Moving load analysis on cross/angle-ply laminated composite nanoplates resting on viscoelastic foundation |
author_facet |
Hai T.; Al-Masoudy M.M.; Alsulamy S.; Hechmi El Ouni M.; Ayvazyan A.; Kumar A. |
author_sort |
Hai T.; Al-Masoudy M.M.; Alsulamy S.; Hechmi El Ouni M.; Ayvazyan A.; Kumar A. |
title |
Moving load analysis on cross/angle-ply laminated composite nanoplates resting on viscoelastic foundation |
title_short |
Moving load analysis on cross/angle-ply laminated composite nanoplates resting on viscoelastic foundation |
title_full |
Moving load analysis on cross/angle-ply laminated composite nanoplates resting on viscoelastic foundation |
title_fullStr |
Moving load analysis on cross/angle-ply laminated composite nanoplates resting on viscoelastic foundation |
title_full_unstemmed |
Moving load analysis on cross/angle-ply laminated composite nanoplates resting on viscoelastic foundation |
title_sort |
Moving load analysis on cross/angle-ply laminated composite nanoplates resting on viscoelastic foundation |
publishDate |
2023 |
container_title |
Composite Structures |
container_volume |
305 |
container_issue |
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doi_str_mv |
10.1016/j.compstruct.2022.116540 |
url |
https://www.scopus.com/inward/record.uri?eid=2-s2.0-85143543828&doi=10.1016%2fj.compstruct.2022.116540&partnerID=40&md5=5f9cd26936d9f686526021206b82ed08 |
description |
In this research contribution, size-dependent forced vibration analysis of embedded cross/angle-plies laminated composite nanoplate in a viscoelastic foundation while subjected to a moving load is investigated. Through Hamiltonian principle, the governing motion equations are derived on the basis of a four-variable refined higher-order shear deformation theory (RHSDT) in Cartesian coordinate and Eringen nonlocal differential model (ENDM) is used in order to predict the size-dependent effects. Afterwards, in order to solve the equations, a time-dependent system of state-space in conjunction with an analytical solution method is implemented over the structures. For the first time, the effect of lay-up numbers and sequences, fiber orientations of involved layers, elastic/viscoelastic foundation coefficients, and nanoplate geometries on the size-dependent dynamic response of laminated composite nanoplate under moving concentrated load with different values of velocity and time history is examined. © 2022 Elsevier Ltd |
publisher |
Elsevier Ltd |
issn |
02638223 |
language |
English |
format |
Article |
accesstype |
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record_format |
scopus |
collection |
Scopus |
_version_ |
1814778503743143936 |