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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| Main Author | |
|---|---|
| Format | Dissertation |
| Language | English |
| Published |
Cranfield University
2013
|
| Online Access | Get full text |
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