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...
Ausführliche Beschreibung

Gespeichert in:

Autor*in:	Zuo, Peng [verfasserIn] Shi, Xianjie [verfasserIn] Ge, Renwei [verfasserIn] Luo, Jingrun [verfasserIn] Ning, Minliang [verfasserIn]

Format:	E-Artikel
Sprache:	Englisch

Erschienen:	2022

Schlagwörter:	Thermal environment Laminated composite cylindrical shell Vibration characteristic Trigonometric series expansion

Übergeordnetes Werk:	Enthalten in: Engineering analysis with boundary elements - Amsterdam [u.a.] : Elsevier Science, 1989, 140, Seite 592-606
Übergeordnetes Werk:	volume:140 ; pages:592-606

DOI / URN:	10.1016/j.enganabound.2022.04.028

Katalog-ID:	ELV007918410

Internformat


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245	1	0	\|a A new meshfree approach for vibration analysis of arbitrary restrained laminated composite cylindrical shell under thermal environment
264		1	\|c 2022
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520			\|a 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.
650		4	\|a Thermal environment
650		4	\|a Laminated composite cylindrical shell
650		4	\|a Vibration characteristic
650		4	\|a Trigonometric series expansion
700	1		\|a Shi, Xianjie \|e verfasserin \|0 (orcid)0000-0001-9758-2403 \|4 aut
700	1		\|a Ge, Renwei \|e verfasserin \|4 aut
700	1		\|a Luo, Jingrun \|e verfasserin \|4 aut
700	1		\|a Ning, Minliang \|e verfasserin \|4 aut
773	0	8	\|i Enthalten in \|t Engineering analysis with boundary elements \|d Amsterdam [u.a.] : Elsevier Science, 1989 \|g 140, Seite 592-606 \|h Online-Ressource \|w (DE-627)320515486 \|w (DE-600)2013898-2 \|w (DE-576)259271462 \|x 0955-7997 \|7 nnns
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912			\|a GBV_ILN_69
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912			\|a GBV_ILN_73
912			\|a GBV_ILN_74
912			\|a GBV_ILN_90
912			\|a GBV_ILN_95
912			\|a GBV_ILN_100
912			\|a GBV_ILN_105
912			\|a GBV_ILN_110
912			\|a GBV_ILN_150
912			\|a GBV_ILN_151
912			\|a GBV_ILN_224
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912			\|a GBV_ILN_602
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912			\|a GBV_ILN_2001
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912			\|a GBV_ILN_2025
912			\|a GBV_ILN_2026
912			\|a GBV_ILN_2027
912			\|a GBV_ILN_2034
912			\|a GBV_ILN_2038
912			\|a GBV_ILN_2044
912			\|a GBV_ILN_2048
912			\|a GBV_ILN_2049
912			\|a GBV_ILN_2050
912			\|a GBV_ILN_2055
912			\|a GBV_ILN_2056
912			\|a GBV_ILN_2059
912			\|a GBV_ILN_2061
912			\|a GBV_ILN_2064
912			\|a GBV_ILN_2065
912			\|a GBV_ILN_2068
912			\|a GBV_ILN_2111
912			\|a GBV_ILN_2112
912			\|a GBV_ILN_2113
912			\|a GBV_ILN_2118
912			\|a GBV_ILN_2122
912			\|a GBV_ILN_2129
912			\|a GBV_ILN_2143
912			\|a GBV_ILN_2147
912			\|a GBV_ILN_2148
912			\|a GBV_ILN_2152
912			\|a GBV_ILN_2153
912			\|a GBV_ILN_2190
912			\|a GBV_ILN_2232
912			\|a GBV_ILN_2336
912			\|a GBV_ILN_2470
912			\|a GBV_ILN_2507
912			\|a GBV_ILN_2522
912			\|a GBV_ILN_4035
912			\|a GBV_ILN_4037
912			\|a GBV_ILN_4046
912			\|a GBV_ILN_4112
912			\|a GBV_ILN_4125
912			\|a GBV_ILN_4126
912			\|a GBV_ILN_4242
912			\|a GBV_ILN_4251
912			\|a GBV_ILN_4305
912			\|a GBV_ILN_4313
912			\|a GBV_ILN_4322
912			\|a GBV_ILN_4323
912			\|a GBV_ILN_4324
912			\|a GBV_ILN_4325
912			\|a GBV_ILN_4326
912			\|a GBV_ILN_4333
912			\|a GBV_ILN_4334
912			\|a GBV_ILN_4335
912			\|a GBV_ILN_4338
912			\|a GBV_ILN_4393
936	b	k	\|a 50.03 \|j Methoden und Techniken der Ingenieurwissenschaften \|q VZ
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952			\|d 140 \|h 592-606

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publishDate	2022
allfields	10.1016/j.enganabound.2022.04.028 doi (DE-627)ELV007918410 (ELSEVIER)S0955-7997(22)00137-0 DE-627 ger DE-627 rda eng 690 620 VZ 50.03 bkl Zuo, Peng verfasserin aut A new meshfree approach for vibration analysis of arbitrary restrained laminated composite cylindrical shell under thermal environment 2022 nicht spezifiziert zzz rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier 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. Thermal environment Laminated composite cylindrical shell Vibration characteristic Trigonometric series expansion Shi, Xianjie verfasserin (orcid)0000-0001-9758-2403 aut Ge, Renwei verfasserin aut Luo, Jingrun verfasserin aut Ning, Minliang verfasserin aut Enthalten in Engineering analysis with boundary elements Amsterdam [u.a.] : Elsevier Science, 1989 140, Seite 592-606 Online-Ressource (DE-627)320515486 (DE-600)2013898-2 (DE-576)259271462 0955-7997 nnns volume:140 pages:592-606 GBV_USEFLAG_U GBV_ELV SYSFLAG_U GBV_ILN_20 GBV_ILN_22 GBV_ILN_23 GBV_ILN_24 GBV_ILN_31 GBV_ILN_32 GBV_ILN_40 GBV_ILN_60 GBV_ILN_62 GBV_ILN_63 GBV_ILN_65 GBV_ILN_69 GBV_ILN_70 GBV_ILN_73 GBV_ILN_74 GBV_ILN_90 GBV_ILN_95 GBV_ILN_100 GBV_ILN_105 GBV_ILN_110 GBV_ILN_150 GBV_ILN_151 GBV_ILN_224 GBV_ILN_370 GBV_ILN_602 GBV_ILN_702 GBV_ILN_2001 GBV_ILN_2003 GBV_ILN_2004 GBV_ILN_2005 GBV_ILN_2006 GBV_ILN_2008 GBV_ILN_2010 GBV_ILN_2011 GBV_ILN_2014 GBV_ILN_2015 GBV_ILN_2020 GBV_ILN_2021 GBV_ILN_2025 GBV_ILN_2026 GBV_ILN_2027 GBV_ILN_2034 GBV_ILN_2038 GBV_ILN_2044 GBV_ILN_2048 GBV_ILN_2049 GBV_ILN_2050 GBV_ILN_2055 GBV_ILN_2056 GBV_ILN_2059 GBV_ILN_2061 GBV_ILN_2064 GBV_ILN_2065 GBV_ILN_2068 GBV_ILN_2111 GBV_ILN_2112 GBV_ILN_2113 GBV_ILN_2118 GBV_ILN_2122 GBV_ILN_2129 GBV_ILN_2143 GBV_ILN_2147 GBV_ILN_2148 GBV_ILN_2152 GBV_ILN_2153 GBV_ILN_2190 GBV_ILN_2232 GBV_ILN_2336 GBV_ILN_2470 GBV_ILN_2507 GBV_ILN_2522 GBV_ILN_4035 GBV_ILN_4037 GBV_ILN_4046 GBV_ILN_4112 GBV_ILN_4125 GBV_ILN_4126 GBV_ILN_4242 GBV_ILN_4251 GBV_ILN_4305 GBV_ILN_4313 GBV_ILN_4322 GBV_ILN_4323 GBV_ILN_4324 GBV_ILN_4325 GBV_ILN_4326 GBV_ILN_4333 GBV_ILN_4334 GBV_ILN_4335 GBV_ILN_4338 GBV_ILN_4393 50.03 Methoden und Techniken der Ingenieurwissenschaften VZ AR 140 592-606
spelling	10.1016/j.enganabound.2022.04.028 doi (DE-627)ELV007918410 (ELSEVIER)S0955-7997(22)00137-0 DE-627 ger DE-627 rda eng 690 620 VZ 50.03 bkl Zuo, Peng verfasserin aut A new meshfree approach for vibration analysis of arbitrary restrained laminated composite cylindrical shell under thermal environment 2022 nicht spezifiziert zzz rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier 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. Thermal environment Laminated composite cylindrical shell Vibration characteristic Trigonometric series expansion Shi, Xianjie verfasserin (orcid)0000-0001-9758-2403 aut Ge, Renwei verfasserin aut Luo, Jingrun verfasserin aut Ning, Minliang verfasserin aut Enthalten in Engineering analysis with boundary elements Amsterdam [u.a.] : Elsevier Science, 1989 140, Seite 592-606 Online-Ressource (DE-627)320515486 (DE-600)2013898-2 (DE-576)259271462 0955-7997 nnns volume:140 pages:592-606 GBV_USEFLAG_U GBV_ELV SYSFLAG_U GBV_ILN_20 GBV_ILN_22 GBV_ILN_23 GBV_ILN_24 GBV_ILN_31 GBV_ILN_32 GBV_ILN_40 GBV_ILN_60 GBV_ILN_62 GBV_ILN_63 GBV_ILN_65 GBV_ILN_69 GBV_ILN_70 GBV_ILN_73 GBV_ILN_74 GBV_ILN_90 GBV_ILN_95 GBV_ILN_100 GBV_ILN_105 GBV_ILN_110 GBV_ILN_150 GBV_ILN_151 GBV_ILN_224 GBV_ILN_370 GBV_ILN_602 GBV_ILN_702 GBV_ILN_2001 GBV_ILN_2003 GBV_ILN_2004 GBV_ILN_2005 GBV_ILN_2006 GBV_ILN_2008 GBV_ILN_2010 GBV_ILN_2011 GBV_ILN_2014 GBV_ILN_2015 GBV_ILN_2020 GBV_ILN_2021 GBV_ILN_2025 GBV_ILN_2026 GBV_ILN_2027 GBV_ILN_2034 GBV_ILN_2038 GBV_ILN_2044 GBV_ILN_2048 GBV_ILN_2049 GBV_ILN_2050 GBV_ILN_2055 GBV_ILN_2056 GBV_ILN_2059 GBV_ILN_2061 GBV_ILN_2064 GBV_ILN_2065 GBV_ILN_2068 GBV_ILN_2111 GBV_ILN_2112 GBV_ILN_2113 GBV_ILN_2118 GBV_ILN_2122 GBV_ILN_2129 GBV_ILN_2143 GBV_ILN_2147 GBV_ILN_2148 GBV_ILN_2152 GBV_ILN_2153 GBV_ILN_2190 GBV_ILN_2232 GBV_ILN_2336 GBV_ILN_2470 GBV_ILN_2507 GBV_ILN_2522 GBV_ILN_4035 GBV_ILN_4037 GBV_ILN_4046 GBV_ILN_4112 GBV_ILN_4125 GBV_ILN_4126 GBV_ILN_4242 GBV_ILN_4251 GBV_ILN_4305 GBV_ILN_4313 GBV_ILN_4322 GBV_ILN_4323 GBV_ILN_4324 GBV_ILN_4325 GBV_ILN_4326 GBV_ILN_4333 GBV_ILN_4334 GBV_ILN_4335 GBV_ILN_4338 GBV_ILN_4393 50.03 Methoden und Techniken der Ingenieurwissenschaften VZ AR 140 592-606
allfields_unstemmed	10.1016/j.enganabound.2022.04.028 doi (DE-627)ELV007918410 (ELSEVIER)S0955-7997(22)00137-0 DE-627 ger DE-627 rda eng 690 620 VZ 50.03 bkl Zuo, Peng verfasserin aut A new meshfree approach for vibration analysis of arbitrary restrained laminated composite cylindrical shell under thermal environment 2022 nicht spezifiziert zzz rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier 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. Thermal environment Laminated composite cylindrical shell Vibration characteristic Trigonometric series expansion Shi, Xianjie verfasserin (orcid)0000-0001-9758-2403 aut Ge, Renwei verfasserin aut Luo, Jingrun verfasserin aut Ning, Minliang verfasserin aut Enthalten in Engineering analysis with boundary elements Amsterdam [u.a.] : Elsevier Science, 1989 140, Seite 592-606 Online-Ressource (DE-627)320515486 (DE-600)2013898-2 (DE-576)259271462 0955-7997 nnns volume:140 pages:592-606 GBV_USEFLAG_U GBV_ELV SYSFLAG_U GBV_ILN_20 GBV_ILN_22 GBV_ILN_23 GBV_ILN_24 GBV_ILN_31 GBV_ILN_32 GBV_ILN_40 GBV_ILN_60 GBV_ILN_62 GBV_ILN_63 GBV_ILN_65 GBV_ILN_69 GBV_ILN_70 GBV_ILN_73 GBV_ILN_74 GBV_ILN_90 GBV_ILN_95 GBV_ILN_100 GBV_ILN_105 GBV_ILN_110 GBV_ILN_150 GBV_ILN_151 GBV_ILN_224 GBV_ILN_370 GBV_ILN_602 GBV_ILN_702 GBV_ILN_2001 GBV_ILN_2003 GBV_ILN_2004 GBV_ILN_2005 GBV_ILN_2006 GBV_ILN_2008 GBV_ILN_2010 GBV_ILN_2011 GBV_ILN_2014 GBV_ILN_2015 GBV_ILN_2020 GBV_ILN_2021 GBV_ILN_2025 GBV_ILN_2026 GBV_ILN_2027 GBV_ILN_2034 GBV_ILN_2038 GBV_ILN_2044 GBV_ILN_2048 GBV_ILN_2049 GBV_ILN_2050 GBV_ILN_2055 GBV_ILN_2056 GBV_ILN_2059 GBV_ILN_2061 GBV_ILN_2064 GBV_ILN_2065 GBV_ILN_2068 GBV_ILN_2111 GBV_ILN_2112 GBV_ILN_2113 GBV_ILN_2118 GBV_ILN_2122 GBV_ILN_2129 GBV_ILN_2143 GBV_ILN_2147 GBV_ILN_2148 GBV_ILN_2152 GBV_ILN_2153 GBV_ILN_2190 GBV_ILN_2232 GBV_ILN_2336 GBV_ILN_2470 GBV_ILN_2507 GBV_ILN_2522 GBV_ILN_4035 GBV_ILN_4037 GBV_ILN_4046 GBV_ILN_4112 GBV_ILN_4125 GBV_ILN_4126 GBV_ILN_4242 GBV_ILN_4251 GBV_ILN_4305 GBV_ILN_4313 GBV_ILN_4322 GBV_ILN_4323 GBV_ILN_4324 GBV_ILN_4325 GBV_ILN_4326 GBV_ILN_4333 GBV_ILN_4334 GBV_ILN_4335 GBV_ILN_4338 GBV_ILN_4393 50.03 Methoden und Techniken der Ingenieurwissenschaften VZ AR 140 592-606
allfieldsGer	10.1016/j.enganabound.2022.04.028 doi (DE-627)ELV007918410 (ELSEVIER)S0955-7997(22)00137-0 DE-627 ger DE-627 rda eng 690 620 VZ 50.03 bkl Zuo, Peng verfasserin aut A new meshfree approach for vibration analysis of arbitrary restrained laminated composite cylindrical shell under thermal environment 2022 nicht spezifiziert zzz rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier 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. Thermal environment Laminated composite cylindrical shell Vibration characteristic Trigonometric series expansion Shi, Xianjie verfasserin (orcid)0000-0001-9758-2403 aut Ge, Renwei verfasserin aut Luo, Jingrun verfasserin aut Ning, Minliang verfasserin aut Enthalten in Engineering analysis with boundary elements Amsterdam [u.a.] : Elsevier Science, 1989 140, Seite 592-606 Online-Ressource (DE-627)320515486 (DE-600)2013898-2 (DE-576)259271462 0955-7997 nnns volume:140 pages:592-606 GBV_USEFLAG_U GBV_ELV SYSFLAG_U GBV_ILN_20 GBV_ILN_22 GBV_ILN_23 GBV_ILN_24 GBV_ILN_31 GBV_ILN_32 GBV_ILN_40 GBV_ILN_60 GBV_ILN_62 GBV_ILN_63 GBV_ILN_65 GBV_ILN_69 GBV_ILN_70 GBV_ILN_73 GBV_ILN_74 GBV_ILN_90 GBV_ILN_95 GBV_ILN_100 GBV_ILN_105 GBV_ILN_110 GBV_ILN_150 GBV_ILN_151 GBV_ILN_224 GBV_ILN_370 GBV_ILN_602 GBV_ILN_702 GBV_ILN_2001 GBV_ILN_2003 GBV_ILN_2004 GBV_ILN_2005 GBV_ILN_2006 GBV_ILN_2008 GBV_ILN_2010 GBV_ILN_2011 GBV_ILN_2014 GBV_ILN_2015 GBV_ILN_2020 GBV_ILN_2021 GBV_ILN_2025 GBV_ILN_2026 GBV_ILN_2027 GBV_ILN_2034 GBV_ILN_2038 GBV_ILN_2044 GBV_ILN_2048 GBV_ILN_2049 GBV_ILN_2050 GBV_ILN_2055 GBV_ILN_2056 GBV_ILN_2059 GBV_ILN_2061 GBV_ILN_2064 GBV_ILN_2065 GBV_ILN_2068 GBV_ILN_2111 GBV_ILN_2112 GBV_ILN_2113 GBV_ILN_2118 GBV_ILN_2122 GBV_ILN_2129 GBV_ILN_2143 GBV_ILN_2147 GBV_ILN_2148 GBV_ILN_2152 GBV_ILN_2153 GBV_ILN_2190 GBV_ILN_2232 GBV_ILN_2336 GBV_ILN_2470 GBV_ILN_2507 GBV_ILN_2522 GBV_ILN_4035 GBV_ILN_4037 GBV_ILN_4046 GBV_ILN_4112 GBV_ILN_4125 GBV_ILN_4126 GBV_ILN_4242 GBV_ILN_4251 GBV_ILN_4305 GBV_ILN_4313 GBV_ILN_4322 GBV_ILN_4323 GBV_ILN_4324 GBV_ILN_4325 GBV_ILN_4326 GBV_ILN_4333 GBV_ILN_4334 GBV_ILN_4335 GBV_ILN_4338 GBV_ILN_4393 50.03 Methoden und Techniken der Ingenieurwissenschaften VZ AR 140 592-606
allfieldsSound	10.1016/j.enganabound.2022.04.028 doi (DE-627)ELV007918410 (ELSEVIER)S0955-7997(22)00137-0 DE-627 ger DE-627 rda eng 690 620 VZ 50.03 bkl Zuo, Peng verfasserin aut A new meshfree approach for vibration analysis of arbitrary restrained laminated composite cylindrical shell under thermal environment 2022 nicht spezifiziert zzz rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier 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. Thermal environment Laminated composite cylindrical shell Vibration characteristic Trigonometric series expansion Shi, Xianjie verfasserin (orcid)0000-0001-9758-2403 aut Ge, Renwei verfasserin aut Luo, Jingrun verfasserin aut Ning, Minliang verfasserin aut Enthalten in Engineering analysis with boundary elements Amsterdam [u.a.] : Elsevier Science, 1989 140, Seite 592-606 Online-Ressource (DE-627)320515486 (DE-600)2013898-2 (DE-576)259271462 0955-7997 nnns volume:140 pages:592-606 GBV_USEFLAG_U GBV_ELV SYSFLAG_U GBV_ILN_20 GBV_ILN_22 GBV_ILN_23 GBV_ILN_24 GBV_ILN_31 GBV_ILN_32 GBV_ILN_40 GBV_ILN_60 GBV_ILN_62 GBV_ILN_63 GBV_ILN_65 GBV_ILN_69 GBV_ILN_70 GBV_ILN_73 GBV_ILN_74 GBV_ILN_90 GBV_ILN_95 GBV_ILN_100 GBV_ILN_105 GBV_ILN_110 GBV_ILN_150 GBV_ILN_151 GBV_ILN_224 GBV_ILN_370 GBV_ILN_602 GBV_ILN_702 GBV_ILN_2001 GBV_ILN_2003 GBV_ILN_2004 GBV_ILN_2005 GBV_ILN_2006 GBV_ILN_2008 GBV_ILN_2010 GBV_ILN_2011 GBV_ILN_2014 GBV_ILN_2015 GBV_ILN_2020 GBV_ILN_2021 GBV_ILN_2025 GBV_ILN_2026 GBV_ILN_2027 GBV_ILN_2034 GBV_ILN_2038 GBV_ILN_2044 GBV_ILN_2048 GBV_ILN_2049 GBV_ILN_2050 GBV_ILN_2055 GBV_ILN_2056 GBV_ILN_2059 GBV_ILN_2061 GBV_ILN_2064 GBV_ILN_2065 GBV_ILN_2068 GBV_ILN_2111 GBV_ILN_2112 GBV_ILN_2113 GBV_ILN_2118 GBV_ILN_2122 GBV_ILN_2129 GBV_ILN_2143 GBV_ILN_2147 GBV_ILN_2148 GBV_ILN_2152 GBV_ILN_2153 GBV_ILN_2190 GBV_ILN_2232 GBV_ILN_2336 GBV_ILN_2470 GBV_ILN_2507 GBV_ILN_2522 GBV_ILN_4035 GBV_ILN_4037 GBV_ILN_4046 GBV_ILN_4112 GBV_ILN_4125 GBV_ILN_4126 GBV_ILN_4242 GBV_ILN_4251 GBV_ILN_4305 GBV_ILN_4313 GBV_ILN_4322 GBV_ILN_4323 GBV_ILN_4324 GBV_ILN_4325 GBV_ILN_4326 GBV_ILN_4333 GBV_ILN_4334 GBV_ILN_4335 GBV_ILN_4338 GBV_ILN_4393 50.03 Methoden und Techniken der Ingenieurwissenschaften VZ AR 140 592-606
language	English
source	Enthalten in Engineering analysis with boundary elements 140, Seite 592-606 volume:140 pages:592-606
sourceStr	Enthalten in Engineering analysis with boundary elements 140, Seite 592-606 volume:140 pages:592-606
format_phy_str_mv	Article
bklname	Methoden und Techniken der Ingenieurwissenschaften
institution	findex.gbv.de
topic_facet	Thermal environment Laminated composite cylindrical shell Vibration characteristic Trigonometric series expansion
dewey-raw	690
isfreeaccess_bool	false
container_title	Engineering analysis with boundary elements
authorswithroles_txt_mv	Zuo, Peng @@aut@@ Shi, Xianjie @@aut@@ Ge, Renwei @@aut@@ Luo, Jingrun @@aut@@ Ning, Minliang @@aut@@
publishDateDaySort_date	2022-01-01T00:00:00Z
hierarchy_top_id	320515486
dewey-sort	3690
id	ELV007918410
language_de	englisch
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author	Zuo, Peng
spellingShingle	Zuo, Peng ddc 690 bkl 50.03 misc Thermal environment misc Laminated composite cylindrical shell misc Vibration characteristic misc Trigonometric series expansion A new meshfree approach for vibration analysis of arbitrary restrained laminated composite cylindrical shell under thermal environment
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topic_title	690 620 VZ 50.03 bkl A new meshfree approach for vibration analysis of arbitrary restrained laminated composite cylindrical shell under thermal environment Thermal environment Laminated composite cylindrical shell Vibration characteristic Trigonometric series expansion
topic	ddc 690 bkl 50.03 misc Thermal environment misc Laminated composite cylindrical shell misc Vibration characteristic misc Trigonometric series expansion
topic_unstemmed	ddc 690 bkl 50.03 misc Thermal environment misc Laminated composite cylindrical shell misc Vibration characteristic misc Trigonometric series expansion
topic_browse	ddc 690 bkl 50.03 misc Thermal environment misc Laminated composite cylindrical shell misc Vibration characteristic misc Trigonometric series expansion
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title	A new meshfree approach for vibration analysis of arbitrary restrained laminated composite cylindrical shell under thermal environment
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title_full	A new meshfree approach for vibration analysis of arbitrary restrained laminated composite cylindrical shell under thermal environment
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title_sort	a new meshfree approach for vibration analysis of arbitrary restrained laminated composite cylindrical shell under thermal environment
title_auth	A new meshfree approach for vibration analysis of arbitrary restrained laminated composite cylindrical shell under thermal environment
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.
abstractGer	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.
abstract_unstemmed	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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title_short	A new meshfree approach for vibration analysis of arbitrary restrained laminated composite cylindrical shell under thermal environment
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author2	Shi, Xianjie Ge, Renwei Luo, Jingrun Ning, Minliang
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doi_str	10.1016/j.enganabound.2022.04.028
up_date	2024-07-06T17:55:03.327Z
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A new meshfree approach for vibration analysis of arbitrary restrained laminated composite cylindrical shell under thermal environment

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