On Aerodynamic and Aeroelastic Modeling for Aircraft Design
The work presented in this thesis was performed with the aim of developing improved prediction methods for aerodynamic and aeroelastic analysis to be used in aircraft design. The first part of the thesis concerns the development of a viscous-inviscid interaction model for steady aerodynamic predicti...
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| Format: | Doctoral Thesis |
| Language: | English |
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KTH, Flygdynamik
2017
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| Online Access: | http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-212051 http://nbn-resolving.de/urn:isbn:978-91-7729-480-1 |