Simulating Bird Strike on Aircraft Composite Wing Leading Edge.
In this master thesis project the possibility to model the response of a wing when subjected to bird strike using finite elements is analyzed. Since this transient event lasts only a few milliseconds the used solution method is explicit time integration. The wing is manufactured using carbon fiber l...
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| Format: | Others |
| Language: | English |
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KTH, Hållfasthetslära (Inst.)
2012
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| Online Access: | http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-103783 |