Effect of an external vortex on the uav aerodynamic performances
In this present work, the CFD and wind tunnel are used to investigate the effect of an external vortex around an UAV in order to obtain initial estimates of lift and drag coefficients with flow velocity of 30 meters per second for various angles of attack. The model of Spalart- Allmaras turbulen...
| Main Authors: | , , , |
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| Format: | Article |
| Language: | English |
| Published: |
EDP Sciences
2012-06-01
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| Series: | EPJ Web of Conferences |
| Subjects: | |
| Online Access: | http://dx.doi.org/10.1051/epjconf/20122501104 |