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Modelling of bird strike on an aircraft wing leading edge made from fibre metal laminates - Part 1: Material modelling

Publication status:: Published

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APA Style

McCarthy, M., Xiao, J. R., Petrinic, N., Kamoulakos, A., & Melito, V. (2004). Modelling of bird strike on an aircraft wing leading edge made from fibre metal laminates - Part 1: Material modelling. APPLIED COMPOSITE MATERIALS, 11(5), 295–315.

MLA Style

McCarthy, M., et al. “Modelling of Bird Strike on an Aircraft Wing Leading Edge Made from Fibre Metal Laminates - Part 1: Material Modelling.” APPLIED COMPOSITE MATERIALS, vol. 11, no. 5, 2004, pp. 295–315.

Chicago Style

McCarthy, M, JR Xiao, N Petrinic, A Kamoulakos, and V Melito. 2004. “Modelling of Bird Strike on an Aircraft Wing Leading Edge Made from Fibre Metal Laminates - Part 1: Material Modelling.” APPLIED COMPOSITE MATERIALS 11 (5): 295–315.
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Publisher copy:: 10.1023/B:ACMA.0000037133.64496.13

Authors

+ McCarthy, M More by this author

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Author

+ Xiao, JR More by this author

Role:

Author

+ Petrinic, N More by this author

Institution:

University of Oxford

Division:

MPLS

Department:

Engineering Science

Role:

Author

+ Kamoulakos, A More by this author

Role:

Author

+ Melito, V More by this author

Role:

Author

Bibliographic Details

Journal:: APPLIED COMPOSITE MATERIALS
Volume:: 11
Issue:: 5
Pages:: 295-315
Publication date:: 2004-09-01
DOI:: 10.1023/B:ACMA.0000037133.64496.13
ISSN:: 0929-189X

Item Description

Keywords:: strain rate effects

aircraft leading edge

continuum damage mechanics

finite element analysis

fibre metal laminate

bird strike
Pubs id:: pubs:64628
UUID:: uuid:624d56d8-6b21-4dce-b4a7-036567877ea9
Local pid:: pubs:64628
Source identifiers:: 64628
Deposit date:: 2013-11-16

Terms of use

Copyright date:: 2004

Licence:: Terms and Conditions of Use for Oxford University Research Archive

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