Maximum buckling load design of general cross-section cylinders using lamination parameters

A Khani; MM Abdalla; Z Gurdal

Maximum buckling load design of general cross-section cylinders using lamination parameters

A Khani, MM Abdalla, Z Gurdal

Research output: Chapter in Book/Conference proceedings/Edited volume › Conference contribution › Scientific › peer-review

3 Citations (Scopus)

Original language	English
Title of host publication	Proceedings of the 13th AIAA/ISSMO Multidisciplinary Analysis Optimization Conference
Editors	s.n.
Place of Publication	Fort Worth,Texas, USA
Publisher	American Institute of Aeronautics and Astronautics Inc. (AIAA)
Pages	1-13
Number of pages	13
Publication status	Published - 2010
Event	13th AIAA / ISSMO Multidisciplinary Analysis Optimization Conference - Fort Worth,Texas, USA Duration: 13 Sept 2010 → 15 Sept 2010

Publication series

Name
Publisher	AIAA

Conference

Conference	13th AIAA / ISSMO Multidisciplinary Analysis Optimization Conference
Period	13/09/10 → 15/09/10

Keywords

Conf.proc. > 3 pag

Cite this

@inproceedings{74396081e7974b9b95720cbf9ed2f083,

title = "Maximum buckling load design of general cross-section cylinders using lamination parameters",

keywords = "Conf.proc. > 3 pag",

author = "A Khani and MM Abdalla and Z Gurdal",

year = "2010",

language = "English",

publisher = "American Institute of Aeronautics and Astronautics Inc. (AIAA)",

pages = "1--13",

editor = "s.n.",

booktitle = "Proceedings of the 13th AIAA/ISSMO Multidisciplinary Analysis Optimization Conference",

address = "United States",

note = "13th AIAA / ISSMO Multidisciplinary Analysis Optimization Conference ; Conference date: 13-09-2010 Through 15-09-2010",

}

Khani, A, Abdalla, MM & Gurdal, Z 2010, Maximum buckling load design of general cross-section cylinders using lamination parameters. in s.n. (ed.), Proceedings of the 13th AIAA/ISSMO Multidisciplinary Analysis Optimization Conference. American Institute of Aeronautics and Astronautics Inc. (AIAA), Fort Worth,Texas, USA, pp. 1-13, 13th AIAA / ISSMO Multidisciplinary Analysis Optimization Conference, 13/09/10.

Maximum buckling load design of general cross-section cylinders using lamination parameters. / Khani, A; Abdalla, MM; Gurdal, Z.
Proceedings of the 13th AIAA/ISSMO Multidisciplinary Analysis Optimization Conference. ed. / s.n. Fort Worth,Texas, USA: American Institute of Aeronautics and Astronautics Inc. (AIAA), 2010. p. 1-13.

Research output: Chapter in Book/Conference proceedings/Edited volume › Conference contribution › Scientific › peer-review

TY - GEN

T1 - Maximum buckling load design of general cross-section cylinders using lamination parameters

AU - Khani, A

AU - Abdalla, MM

AU - Gurdal, Z

PY - 2010

Y1 - 2010

KW - Conf.proc. > 3 pag

M3 - Conference contribution

SP - 1

EP - 13

BT - Proceedings of the 13th AIAA/ISSMO Multidisciplinary Analysis Optimization Conference

A2 - s.n., null

PB - American Institute of Aeronautics and Astronautics Inc. (AIAA)

CY - Fort Worth,Texas, USA

T2 - 13th AIAA / ISSMO Multidisciplinary Analysis Optimization Conference

Y2 - 13 September 2010 through 15 September 2010

ER -