Modelling bird impacts on an aircraft wing - Part 1: Material modelling of the fibre metal laminate leading edge material with continuum damage mechanics

International Journal of Crashworthiness

Volumn 10, Issue 1, 2005, Pages 41-49

  McCarthy, Michael A ^a   Xiao, J R ^b   Petrinic, N ^c   Kamoulakos, A ^d   Melito, V ^e  

^a UNIVERSITY OF LIMERICK   (Ireland)

^b UNIVERSITY OF DELAWARE   (United States)

^c UNIVERSITY OF OXFORD   (United Kingdom)

^d ESI GROUP   (France)

^e ALENIA SPAZIO   (Italy)

Author keywords

Aircraft leading edge; Bird strike; Continuum damage mechanics; Fibre Metal Laminate

Indexed keywords

EID: 13444262253     PISSN: 13588265     EISSN: None     Source Type: Journal    
DOI: 10.1533/ijcr.2005.0324     Document Type: Article

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