Birdstrike analysis on leading edge of an aircraft wing using a smooth particle hydrodynamics bird model
Birdstrikes on aircraft pose a major threat to human life and there is a need to devolop structures which have high resistance towards these structures. According to the Federal Aviation Regulation (FAR 25.571) on Damage-tolerance and fatigue evaluation of structure (Amdt.25-96), an airplane must be...
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| Format: | Others |
| Language: | en_US |
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Wichita State University
2010
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| Online Access: | http://hdl.handle.net/10057/3339 |