Modelling of bird strike on an aircraft wing leading edge made from fibre metal laminates - Part 2: Modelling of impact with SPH bird model

Applied Composite Materials

Volumn 11, Issue 5, 2004, Pages 317-340

  McCarthy, M A ^a   Xiao, J R ^b   McCarthy, C T ^c   Kamoulakos, A ^d   Ramos, J ^d   Gallard, J P ^e   Melito, V ^f  

^a UNIVERSITY OF LIMERICK   (Ireland)

^b UNIVERSITY OF DELAWARE   (United States)

^c UNIVERSITY COLLEGE DUBLIN   (Ireland)

^d ESI GROUP   (France)

^e CEAT   (France)

^f ALENIA SPAZIO   (Italy)

Author keywords

Aircraft wing leading edge; Bird strike; Fibre metal laminate; Finite element analysis; Smooth particle hydrodynamics

Indexed keywords

AIRCRAFT MODELS; AIRPORT RUNWAYS; ALUMINUM ALLOYS; DEBRIS; FIBERS; FINITE ELEMENT METHOD; HYDRODYNAMICS; LAMINATES; STRENGTH OF MATERIALS;

AIRCRAFT LEADING EDGE; BIRD STRIKES; FIBER METAL LAMINATES; SMOOTH PARTICLE HYDRODYNAMICS;

WINGS;

EID: 4143149879     PISSN: 0929189X     EISSN: None     Source Type: Journal    
DOI: 10.1023/B:ACMA.0000037134.93410.c0     Document Type: Article

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