Buckling Behavior of Optimal Laminated Composite Cylindrical Shells Subjected to Axial Compression and External Pressure

Behzad Abdi; Hamid Mozafari; Amran Ayob; Roya Kohandeld; Ali Alibeigloo

doi:10.4028/www.scientific.net/AMM.121-126.48

Buckling Behavior of Optimal Laminated Composite Cylindrical Shells Subjected to Axial Compression and External Pressure

Behzad Abdi, Hamid Mozafari, Amran Ayob, Roya Kohandeld, Ali Alibeigloo

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

3 Citations (Scopus)

Abstract

In this study, the buckling behavior of optimum laminated composite cylindrical shells subjected to axial compression and external pressure are studied. The cylindrical shells are composed of multi orthotropic layers that the principal axis gets along with the shell axis (x). The number of layers and the fiber orientation of layers are selected as optimization design variables with the aim to find the optimal laminated composite cylindrical shells. The optimization procedure was formulated with the objective of finding the highest buckling pressure. The Genetic Algorithm (GA) and Imperialist Competitive Algorithm (ICA) are two optimization algorithms that are used in this optimization procedure and the results were compared. Also, the effect of materials properties on buckling behavior was analyzed and studied.

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	48-54
Number of pages	7
ISBN (Electronic)	9783037951071, 9783038137153
ISBN (Print)	9783037852828
DOIs	https://doi.org/10.4028/www.scientific.net/AMM.121-126.48
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.

Access to Document

10.4028/www.scientific.net/AMM.121-126.48

Cite this

Abdi, B., Mozafari, H., Ayob, A., Kohandeld, R., & Alibeigloo, A. (2011). Buckling Behavior of Optimal Laminated Composite Cylindrical Shells Subjected to Axial Compression and External Pressure. In D. Sun, W.-P. Sung, & R. Chen (Eds.), Frontiers of Manufacturing and Design Science II (pp. 48-54). (Applied Mechanics and Materials; Vol. 121-126). Trans Tech Publications Ltd. https://doi.org/10.4028/www.scientific.net/AMM.121-126.48

@inproceedings{9721cbd85b354057951b24a29452464d,

title = "Buckling Behavior of Optimal Laminated Composite Cylindrical Shells Subjected to Axial Compression and External Pressure",

abstract = "In this study, the buckling behavior of optimum laminated composite cylindrical shells subjected to axial compression and external pressure are studied. The cylindrical shells are composed of multi orthotropic layers that the principal axis gets along with the shell axis (x). The number of layers and the fiber orientation of layers are selected as optimization design variables with the aim to find the optimal laminated composite cylindrical shells. The optimization procedure was formulated with the objective of finding the highest buckling pressure. The Genetic Algorithm (GA) and Imperialist Competitive Algorithm (ICA) are two optimization algorithms that are used in this optimization procedure and the results were compared. Also, the effect of materials properties on buckling behavior was analyzed and studied.",

keywords = "Buckling, Composite, Cylindrical shell, Genetic algorithm, Imperialist competitive Algorithm",

author = "Behzad Abdi and Hamid Mozafari and Amran Ayob and Roya Kohandeld and Ali Alibeigloo",

year = "2011",

month = oct,

day = "24",

doi = "10.4028/www.scientific.net/AMM.121-126.48",

language = "English",

isbn = "9783037852828",

series = "Applied Mechanics and Materials",

publisher = "Trans Tech Publications Ltd",

pages = "48--54",

editor = "Dongye Sun and Wen-Pei Sung and Ran Chen",

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

address = "Switzerland",

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

url = "https://www.scientific.net/book/frontiers-of-manufacturing-and-design-science-ii/978-3-03813-715-3\#:\textasciitilde{}:text=Selected,\%20peer\%20reviewed\%20papers\%20from\%20the\%20Second,Design\%20Science,\%20(ICFMD\%202011),\%20December\%2011-13,\%20Taiwan.",

}

Abdi, B, Mozafari, H, Ayob, A, Kohandeld, R & Alibeigloo, A 2011, Buckling Behavior of Optimal Laminated Composite Cylindrical Shells Subjected to Axial Compression and External Pressure. 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. 48-54, 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.121-126.48

Buckling Behavior of Optimal Laminated Composite Cylindrical Shells Subjected to Axial Compression and External Pressure. / 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. 48-54 (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 Optimal Laminated Composite Cylindrical Shells Subjected to Axial Compression and External Pressure

AU - Abdi, Behzad

AU - Mozafari, Hamid

AU - Ayob, Amran

AU - Kohandeld, Roya

AU - Alibeigloo, Ali

PY - 2011/10/24

Y1 - 2011/10/24

N2 - In this study, the buckling behavior of optimum laminated composite cylindrical shells subjected to axial compression and external pressure are studied. The cylindrical shells are composed of multi orthotropic layers that the principal axis gets along with the shell axis (x). The number of layers and the fiber orientation of layers are selected as optimization design variables with the aim to find the optimal laminated composite cylindrical shells. The optimization procedure was formulated with the objective of finding the highest buckling pressure. The Genetic Algorithm (GA) and Imperialist Competitive Algorithm (ICA) are two optimization algorithms that are used in this optimization procedure and the results were compared. Also, the effect of materials properties on buckling behavior was analyzed and studied.

AB - In this study, the buckling behavior of optimum laminated composite cylindrical shells subjected to axial compression and external pressure are studied. The cylindrical shells are composed of multi orthotropic layers that the principal axis gets along with the shell axis (x). The number of layers and the fiber orientation of layers are selected as optimization design variables with the aim to find the optimal laminated composite cylindrical shells. The optimization procedure was formulated with the objective of finding the highest buckling pressure. The Genetic Algorithm (GA) and Imperialist Competitive Algorithm (ICA) are two optimization algorithms that are used in this optimization procedure and the results were compared. Also, the effect of materials properties on buckling behavior was analyzed and studied.

KW - Buckling

KW - Composite

KW - Cylindrical shell

KW - Genetic algorithm

KW - Imperialist competitive Algorithm

UR - https://www.scopus.com/pages/publications/81255151142

UR - https://www.scientific.net/book/frontiers-of-manufacturing-and-design-science-ii/978-3-03813-715-3

U2 - 10.4028/www.scientific.net/AMM.121-126.48

DO - 10.4028/www.scientific.net/AMM.121-126.48

M3 - Conference contribution

AN - SCOPUS:81255151142

SN - 9783037852828

T3 - Applied Mechanics and Materials

SP - 48

EP - 54

BT - Frontiers of Manufacturing and Design Science II

A2 - Sun, Dongye

A2 - Sung, Wen-Pei

A2 - Chen, Ran

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, Kohandeld R, Alibeigloo A. Buckling Behavior of Optimal Laminated Composite Cylindrical Shells Subjected to Axial Compression and External Pressure. In Sun D, Sung WP, Chen R, editors, Frontiers of Manufacturing and Design Science II. Trans Tech Publications Ltd. 2011. p. 48-54. (Applied Mechanics and Materials). doi: 10.4028/www.scientific.net/AMM.121-126.48

Buckling Behavior of Optimal Laminated Composite Cylindrical Shells Subjected to Axial Compression and External Pressure

Abstract

Publication series

Conference

Access to Document

Other files and links

Fingerprint

Cite this