Solution of a laminated cylindrical shell using an unconstrained third-order theory

Computers & Structures ◽

10.1016/s0045-7949(98)00137-0 ◽

1998 ◽

Vol 69 (3) ◽

pp. 291-303 ◽

Author(s):

S. Di ◽

H. Rothert

Keyword(s):

Cylindrical Shell ◽

Order Theory ◽

Third Order ◽

Laminated Cylindrical Shell

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A global-local higher order theory for multilayered shells and the analysis of laminated cylindrical shell panels

Composite Structures ◽

10.1016/j.compstruct.2007.10.006 ◽

2008 ◽

Vol 84 (4) ◽

pp. 350-361 ◽

Author(s):

Wu Zhen ◽

Chen Wanji

Keyword(s):

Cylindrical Shell ◽

Order Theory ◽

Higher Order ◽

Higher Order Theory ◽

Laminated Cylindrical Shell

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Analytical solutions for vibrations and buckling analysis of laminated composite nanoplates based on third-order theory and strain gradient approach

Composite Structures ◽

10.1016/j.compstruct.2021.114083 ◽

2021 ◽

pp. 114083

Author(s):

Michele Bacciocchi ◽

Angelo Marcello Tarantino

Keyword(s):

Analytical Solutions ◽

Strain Gradient ◽

Laminated Composite ◽

Order Theory ◽

Buckling Analysis ◽

Third Order ◽

Gradient Approach

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Non-linear solution for locally delaminated buckling near the surface of a laminated cylindrical shell under hydrothermal environment

International Journal of Pressure Vessels and Piping ◽

10.1016/s0308-0161(03)00032-2 ◽

2003 ◽

Vol 80 (4) ◽

pp. 243-251 ◽

Author(s):

X. Wang ◽

H.L. Dai

Keyword(s):

Cylindrical Shell ◽

Linear Solution ◽

Hydrothermal Environment ◽

Laminated Cylindrical Shell

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Corrigendum to “Admissible boundary conditions and solutions to internally pressurized thin arbitrarily laminated cylindrical shell boundary-value problems” [Compos. Struct. 86 (2008) 385–400]

Composite Structures ◽

10.1016/j.compstruct.2014.03.018 ◽

2014 ◽

Vol 113 ◽

pp. 508

Author(s):

Reaz A. Chaudhuri ◽

K. Balaraman ◽

Vincent X. Kunukkasseril

Keyword(s):

Cylindrical Shell ◽

Boundary Conditions ◽

Boundary Value Problems ◽

Boundary Value ◽

Shell Boundary ◽

Laminated Cylindrical Shell

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Boundary layer theory for the buckling and postbuckling of an anisotropic laminated cylindrical shell. Part I: Prediction under axial compression

Composite Structures ◽

10.1016/j.compstruct.2007.01.024 ◽

2008 ◽

Vol 82 (3) ◽

pp. 346-361 ◽

Author(s):

Hui-Shen Shen

Keyword(s):

Boundary Layer ◽

Cylindrical Shell ◽

Axial Compression ◽

Boundary Layer Theory ◽

Laminated Cylindrical Shell ◽

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Nonlinear radial breathing vibrations of CFRP laminated cylindrical shell with non-normal boundary conditions subjected to axial pressure and radial line load at two ends

Composite Structures ◽

10.1016/j.compstruct.2018.01.091 ◽

2018 ◽

Vol 190 ◽

pp. 52-78 ◽

Author(s):

W. Zhang ◽

S.W. Yang ◽

J.J. Mao

Keyword(s):

Cylindrical Shell ◽

Boundary Conditions ◽

Radial Line ◽

Axial Pressure ◽

Line Load ◽

Normal Boundary ◽

Laminated Cylindrical Shell

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Frequency manipulation of a light-activated shape-memory polymer-laminated cylindrical shell

Proceedings of the Institution of Mechanical Engineers Part E Journal of Process Mechanical Engineering ◽

10.1177/09544089211063254 ◽

2021 ◽

pp. 095440892110632

Author(s):

Tao He ◽

Pengpeng Zhu ◽

Xiangmin Zhang

Keyword(s):

Cylindrical Shell ◽

Shape Memory ◽

Natural Frequency ◽

Frequency Control ◽

Shape Memory Polymer ◽

Control Effect ◽

Optimal Scheme ◽

Simply Supported ◽

Control Capability ◽

Laminated Cylindrical Shell

A light-activated shape-memory polymer is a novel smart material that exhibits a dynamic Young's modulus when exposed to light. The non-contact actuation feature facilitates the lamination of a light-activated shape-memory polymer on host structures for realising frequency control. In this study, we investigated the natural frequency of a simply supported cylindrical shell coupled with light-activated shape-memory polymer patches located arbitrarily on the shell. Initially, we compared the natural frequency of a completely laminated cylindrical shell using two different approaches. Further, we analysed the effect of changes in the length and location of the light-activated shape-memory polymer patch pair on the natural frequency of the cylindrical shell. Based on the experimental results, we propose an optimal scheme, wherein several light-activated shape-memory polymer patch pairs are distributed on the surface of the shell, and the frequency control capability of the proposed scheme is evaluated comprehensively. The results verify that the optimal scheme has an adequate control effect on the natural frequency of the cylindrical shell.

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Natural Frequency Optimization of Laminated Cylindrical Shell Subjected to Tsai-Hill Failure Criteria Constraint Using Penalty Method

Advances in Composite Materials and Structures - Key Engineering Materials ◽

10.4028/0-87849-427-8.9 ◽

2007 ◽

pp. 9-12

Author(s):

R. Nabavi ◽

M.H. Yas ◽

Morteza Shakeri

Keyword(s):

Cylindrical Shell ◽

Natural Frequency ◽

Penalty Method ◽

Failure Criteria ◽

Frequency Optimization ◽

Laminated Cylindrical Shell

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Dynamic Analysis of a Functionally Greded Sandwich Beam Traversed by a Moving Mass Based on a Refined Third-Order Theory

10.1007/978-981-16-3239-6_23 ◽

2021 ◽

pp. 301-315

Author(s):

Le Thi Ngoc Anh ◽

Tran Van Lang ◽

Vu Thi An Ninh ◽

Nguyen Dinh Kien

Keyword(s):

Dynamic Analysis ◽

Sandwich Beam ◽

Order Theory ◽

Moving Mass ◽

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Finite Element-based Parametric Investigations of the Stepped-lap Repairs to Laminated Cylindrical Shell with Stiffeners

International Journal of Advancements in Computing Technology ◽

10.4156/ijact.vol4.issue14.11 ◽

2012 ◽

Vol 4 (14) ◽

pp. 83-91

Author(s):

Jia Baohui ◽

Zhao Luchun

Keyword(s):

Finite Element ◽

Cylindrical Shell ◽

Laminated Cylindrical Shell

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