Effect of wing flexibility on aircraft flight dynamics
The purpose of this thesis is to give a preliminary investigation into the effect of wing deformation on flight dynamics. The candidate vehicle is FW-11 which is a flying wing configuration aircraft with high altitude and long endurance characteristics. The aeroelastic effect may be significant for...
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| Language: | en |
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Cranfield University
2012
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| Online Access: | http://dspace.lib.cranfield.ac.uk/handle/1826/7280 |