A first order model of a variable camber wing for a civil passenger aircraft.
This work presents the development, implementation and analysis of a rst order model of a variable camber wing. An aerodynamic model of a homogeneous wing employing variable camber actuation was developed based on the vortex lattice method and was applied to the approach and landing phases (low...
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| Format: | Others |
| Language: | en |
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2012
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| Online Access: | http://hdl.handle.net/10539/11948 |