Predicting the ultimate load of a CFRP wingbox
| Data(s) |
01/07/2004
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|---|---|
| Resumo |
<p>The finite element method in conjunction with the Soutis-Fleck model is used to predict the residual strength after impact of a carbon-fibre reinforced plastic wingbox subjected to a cantilever type loading. The maximum stress failure criterion further validates the Soutis-Fleck model predictions. The Soutis-Fleck model predicts that the wingbox fails at a tip load of 99.2 kN, approximately 5.5% less than the experimental observation</p> |
| Identificador | |
| Idioma(s) |
eng |
| Direitos |
info:eu-repo/semantics/restrictedAccess |
| Fonte |
Koundouros , M , Falzon , B G , Soutis , C & Lord , S J 2004 , ' Predicting the ultimate load of a CFRP wingbox ' Composites Part A: Applied Science and Manufacturing , vol 35 , no. 7-8 , pp. 895-903 . DOI: 10.1016/j.compositesa.2004.01.016 |
| Palavras-Chave | #/dk/atira/pure/subjectarea/asjc/2500/2503 #Ceramics and Composites |
| Tipo |
article |
