Conceptual design and optimization methodology for box wing aircraft
A conceptual design optimization methodology was developed for a medium range box wing aircraft. A baseline conventional cantilever wing aircraft designed for the same mis- sion and payload was also optimized alongside a baseline box wing aircraft. An empirical formula for the mass estimation of the...
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| Language: | en |
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Cranfield University
2013
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| Online Access: | http://dspace.lib.cranfield.ac.uk/handle/1826/7938 |
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