Buckling Behavior of Clamped Laminated Composite Cylindrical Shells under External Pressure Using Finite Element Method

Behzad Abdi; Hamid Mozafari; Amran Ayob; Roya Kohandel

doi:10.4028/www.scientific.net/AMM.121-126.43

Buckling Behavior of Clamped Laminated Composite Cylindrical Shells under External Pressure Using Finite Element Method

Behzad Abdi, Hamid Mozafari, Amran Ayob, Roya Kohandel

University of Technology Malaysia

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution › peer-review

Abstract

In this study, the elastic buckling behavior of clamped laminated composite cylindrical shells under external pressure was studied. The Finite Element Method (FEM) was used to predict the critical elastic buckling pressure behavior when composite cylindrical shells were subjected to external pressure. The edges of the cylindrical shell ends were completely constrained to simulate clamped end conditions. The influences of parameters such as wall thickness, fiber angle, number of layers and L/R ratio of laminated composite cylindrical shells on critical buckling pressure were studied. It has been found that the under external pressure, the thickness and the fiber angle of the layers have the most significant effect on the critical buckling pressure.

Original language	English
Title of host publication	Frontiers of Manufacturing and Design Science II
Editors	Dongye Sun, Wen-Pei Sung, Ran Chen
Publisher	Trans Tech Publications Ltd
Pages	43-47
Number of pages	5
ISBN (Electronic)	9783037951071, 9783038137153
ISBN (Print)	9783037852828
DOIs	https://doi.org/10.4028/www.scientific.net/AMM.121-126.43
Publication status	Published - 24 Oct 2011
Externally published	Yes
Event	2nd International Conference on Frontiers of Manufacturing and Design Science - Taichung, Taiwan, Province of China Duration: 11 Dec 2011 → 13 Dec 2011 https://www.scientific.net/book/frontiers-of-manufacturing-and-design-science-ii/978-3-03813-715-3#:~:text=Selected,%20peer%20reviewed%20papers%20from%20the%20Second,Design%20Science,%20(ICFMD%202011),%20December%2011-13,%20Taiwan.

Publication series

Name	Applied Mechanics and Materials
Publisher	Trans Tech Publications Ltd
Volume	121-126
ISSN (Print)	1660-9336
ISSN (Electronic)	1662-7482

Conference

Conference	2nd International Conference on Frontiers of Manufacturing and Design Science
Abbreviated title	ICFMD 2011
Country/Territory	Taiwan, Province of China
City	Taichung
Period	11/12/11 → 13/12/11
Internet address	https://www.scientific.net/book/frontiers-of-manufacturing-and-design-science-ii/978-3-03813-715-3#:~:text=Selected,%20peer%20reviewed%20papers%20from%20the%20Second,Design%20Science,%20(ICFMD%202011),%20December%2011-13,%20Taiwan.

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10.4028/www.scientific.net/AMM.121-126.43Licence: Unspecified

Cite this

Abdi, B., Mozafari, H., Ayob, A., & Kohandel, R. (2011). Buckling Behavior of Clamped Laminated Composite Cylindrical Shells under External Pressure Using Finite Element Method. In D. Sun, W.-P. Sung, & R. Chen (Eds.), Frontiers of Manufacturing and Design Science II (pp. 43-47). (Applied Mechanics and Materials; Vol. 121-126). Trans Tech Publications Ltd. https://doi.org/10.4028/www.scientific.net/AMM.121-126.43

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title = "Buckling Behavior of Clamped Laminated Composite Cylindrical Shells under External Pressure Using Finite Element Method",

abstract = "In this study, the elastic buckling behavior of clamped laminated composite cylindrical shells under external pressure was studied. The Finite Element Method (FEM) was used to predict the critical elastic buckling pressure behavior when composite cylindrical shells were subjected to external pressure. The edges of the cylindrical shell ends were completely constrained to simulate clamped end conditions. The influences of parameters such as wall thickness, fiber angle, number of layers and L/R ratio of laminated composite cylindrical shells on critical buckling pressure were studied. It has been found that the under external pressure, the thickness and the fiber angle of the layers have the most significant effect on the critical buckling pressure.",

keywords = "Buckling, Clamped, Cylindrical Shell, Finite element analysis, Laminated composite",

author = "Behzad Abdi and Hamid Mozafari and Amran Ayob and Roya Kohandel",

year = "2011",

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doi = "10.4028/www.scientific.net/AMM.121-126.43",

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booktitle = "Frontiers of Manufacturing and Design Science II",

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note = "2nd International Conference on Frontiers of Manufacturing and Design Science, ICFMD 2011 ; Conference date: 11-12-2011 Through 13-12-2011",

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Abdi, B, Mozafari, H, Ayob, A & Kohandel, R 2011, Buckling Behavior of Clamped Laminated Composite Cylindrical Shells under External Pressure Using Finite Element Method. in D Sun, W-P Sung & R Chen (eds), Frontiers of Manufacturing and Design Science II. Applied Mechanics and Materials, vol. 121-126, Trans Tech Publications Ltd, pp. 43-47, 2nd International Conference on Frontiers of Manufacturing and Design Science, Taichung, Taiwan, Province of China, 11/12/11. https://doi.org/10.4028/www.scientific.net/AMM.121-126.43

Buckling Behavior of Clamped Laminated Composite Cylindrical Shells under External Pressure Using Finite Element Method. / Abdi, Behzad; Mozafari, Hamid; Ayob, Amran et al.
Frontiers of Manufacturing and Design Science II. ed. / Dongye Sun; Wen-Pei Sung; Ran Chen. Trans Tech Publications Ltd, 2011. p. 43-47 (Applied Mechanics and Materials; Vol. 121-126).

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution › peer-review

TY - GEN

T1 - Buckling Behavior of Clamped Laminated Composite Cylindrical Shells under External Pressure Using Finite Element Method

AU - Abdi, Behzad

AU - Mozafari, Hamid

AU - Ayob, Amran

AU - Kohandel, Roya

PY - 2011/10/24

Y1 - 2011/10/24

N2 - In this study, the elastic buckling behavior of clamped laminated composite cylindrical shells under external pressure was studied. The Finite Element Method (FEM) was used to predict the critical elastic buckling pressure behavior when composite cylindrical shells were subjected to external pressure. The edges of the cylindrical shell ends were completely constrained to simulate clamped end conditions. The influences of parameters such as wall thickness, fiber angle, number of layers and L/R ratio of laminated composite cylindrical shells on critical buckling pressure were studied. It has been found that the under external pressure, the thickness and the fiber angle of the layers have the most significant effect on the critical buckling pressure.

AB - In this study, the elastic buckling behavior of clamped laminated composite cylindrical shells under external pressure was studied. The Finite Element Method (FEM) was used to predict the critical elastic buckling pressure behavior when composite cylindrical shells were subjected to external pressure. The edges of the cylindrical shell ends were completely constrained to simulate clamped end conditions. The influences of parameters such as wall thickness, fiber angle, number of layers and L/R ratio of laminated composite cylindrical shells on critical buckling pressure were studied. It has been found that the under external pressure, the thickness and the fiber angle of the layers have the most significant effect on the critical buckling pressure.

KW - Buckling

KW - Clamped

KW - Cylindrical Shell

KW - Finite element analysis

KW - Laminated composite

UR - https://www.scopus.com/pages/publications/81255151144

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DO - 10.4028/www.scientific.net/AMM.121-126.43

M3 - Conference contribution

AN - SCOPUS:81255151144

SN - 9783037852828

T3 - Applied Mechanics and Materials

SP - 43

EP - 47

BT - Frontiers of Manufacturing and Design Science II

A2 - Sun, Dongye

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PB - Trans Tech Publications Ltd

T2 - 2nd International Conference on Frontiers of Manufacturing and Design Science

Y2 - 11 December 2011 through 13 December 2011

ER -

Abdi B, Mozafari H, Ayob A, Kohandel R. Buckling Behavior of Clamped Laminated Composite Cylindrical Shells under External Pressure Using Finite Element Method. In Sun D, Sung WP, Chen R, editors, Frontiers of Manufacturing and Design Science II. Trans Tech Publications Ltd. 2011. p. 43-47. (Applied Mechanics and Materials). doi: 10.4028/www.scientific.net/AMM.121-126.43

Buckling Behavior of Clamped Laminated Composite Cylindrical Shells under External Pressure Using Finite Element Method

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