Structural optimization of aircraft lifting surfaces to satisfy flutter requirements
The research reported in this thesis is concerned with the structural weight optimization of aircraft lifting surfaces when subjected to the satisfaction of flutter requirements. The main text is intended primarily as an expository account on the work and as such it aims at introducing and defining...
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| Language: | en |
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Cranfield University
2009
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| Online Access: | http://hdl.handle.net/1826/3657 |
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