Aeroelastic Concepts for Flexible Aircraft Structures
In this thesis, aeroelastic concepts for increased aircraft performance are developed and evaluated. Active aeroelastic concepts are in focus as well as robust analysis concepts aiming at efficient analysis using numerical models with uncertain or varying model parameters. The thesis presents differ...
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| Format: | Doctoral Thesis |
| Language: | English |
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KTH, Farkost och flyg
2007
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| Online Access: | http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-4419 http://nbn-resolving.de/urn:isbn:978-91-7178-706-4 |