A new meshfree approach for vibration analysis of arbitrary restrained laminated composite cylindrical shell under thermal environment
This study presents a new meshfree approach for thermal vibration analysis of laminated composite cylindrical shell subject to arbitrary boundary conditions. The boundaries of laminated structures are constrained by artificial springs with variable stiffness. The spectro-geometric method (SGM) combi...
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| Published in | Engineering analysis with boundary elements Vol. 140; pp. 592 - 606 |
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| Main Authors | , , , , |
| Format | Journal Article |
| Language | English |
| Published |
Elsevier Ltd
01.07.2022
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| Subjects | |
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| Abstract | This study presents a new meshfree approach for thermal vibration analysis of laminated composite cylindrical shell subject to arbitrary boundary conditions. The boundaries of laminated structures are constrained by artificial springs with variable stiffness. The spectro-geometric method (SGM) combined sine/consine functions containing circumferential wavenumber is employed to expand the displacement components of physical system. Following Reissner-Naghdi's thin shell theory, the Lagrangian energy functionals of the studied structure is derived, and the governing equation of laminated composite cylindrical shell under thermal environment is formulated with Rayleigh-Ritz method. After that, the convergence investigation and accuracy examination of the present method are both carried out by performing some numerical case studies. Finally, the effect of some crucial factors including temperature variable, boundary condition, length-radius ratio and laminated layers on the thermal vibration characteristics of laminated composite cylindrical shell are also studied. |
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| AbstractList | This study presents a new meshfree approach for thermal vibration analysis of laminated composite cylindrical shell subject to arbitrary boundary conditions. The boundaries of laminated structures are constrained by artificial springs with variable stiffness. The spectro-geometric method (SGM) combined sine/consine functions containing circumferential wavenumber is employed to expand the displacement components of physical system. Following Reissner-Naghdi's thin shell theory, the Lagrangian energy functionals of the studied structure is derived, and the governing equation of laminated composite cylindrical shell under thermal environment is formulated with Rayleigh-Ritz method. After that, the convergence investigation and accuracy examination of the present method are both carried out by performing some numerical case studies. Finally, the effect of some crucial factors including temperature variable, boundary condition, length-radius ratio and laminated layers on the thermal vibration characteristics of laminated composite cylindrical shell are also studied. |
| Author | Ge, Renwei Ning, Minliang Zuo, Peng Shi, Xianjie Luo, Jingrun |
| Author_xml | – sequence: 1 givenname: Peng surname: Zuo fullname: Zuo, Peng organization: Department of Modern Mechanics, University of Science and Technology of China, Hefei, 230026, P.R. China – sequence: 2 givenname: Xianjie orcidid: 0000-0001-9758-2403 surname: Shi fullname: Shi, Xianjie email: 411shixj@caep.cn organization: Institute of Systems Engineering, China Academy of Engineering Physics, Mianyang, 621999, P.R. China – sequence: 3 givenname: Renwei surname: Ge fullname: Ge, Renwei organization: Institute of Systems Engineering, China Academy of Engineering Physics, Mianyang, 621999, P.R. China – sequence: 4 givenname: Jingrun surname: Luo fullname: Luo, Jingrun organization: Institute of Systems Engineering, China Academy of Engineering Physics, Mianyang, 621999, P.R. China – sequence: 5 givenname: Minliang surname: Ning fullname: Ning, Minliang organization: Institute of Systems Engineering, China Academy of Engineering Physics, Mianyang, 621999, P.R. China |
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| CitedBy_id | crossref_primary_10_1016_j_enganabound_2023_05_004 crossref_primary_10_1016_j_enganabound_2023_05_026 crossref_primary_10_1016_j_tws_2024_111734 crossref_primary_10_1016_j_enganabound_2022_10_021 crossref_primary_10_1142_S0219455423501080 crossref_primary_10_1142_S1758825124500455 crossref_primary_10_1016_j_engstruct_2022_114818 crossref_primary_10_1016_j_oceaneng_2023_114814 crossref_primary_10_1016_j_compstruct_2024_118315 crossref_primary_10_1016_j_istruc_2023_06_018 |
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| Keywords | Trigonometric series expansion Vibration characteristic Laminated composite cylindrical shell Thermal environment |
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| SubjectTerms | Laminated composite cylindrical shell Thermal environment Trigonometric series expansion Vibration characteristic |
| Title | A new meshfree approach for vibration analysis of arbitrary restrained laminated composite cylindrical shell under thermal environment |
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