Optimization of a Composite Wing Subject to Multi Constraints
In this thesis, an investigation has been carried out into a minimum weight optimization analysis of a composite wing with multi design constraints under both static and dynamic loadings. The study includes the influence of a morphing leading edge on the wing stiffness and gust load reduction by emp...
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| Language: | en |
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Cranfield University
2014
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| Online Access: | http://dspace.lib.cranfield.ac.uk/handle/1826/8449 |