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

Publication status:
Published

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Publisher copy:
10.1533/ijcr.2005.0324

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Institution:
University of Oxford
Department:
Oxford, MPLS, Engineering Science
Role:
Author
Journal:
INTERNATIONAL JOURNAL OF CRASHWORTHINESS
Volume:
10
Issue:
1
Pages:
41-49
Publication date:
2005-01-01
DOI:
EISSN:
1754-2111
ISSN:
1358-8265
URN:
uuid:e3e4d8cf-3cf2-4d15-8243-da05b5f420f2
Source identifiers:
64617
Local pid:
pubs:64617

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