Wingtip Vortex Alleviation Using a Reverse Delta Type Add-on Device
<p>The result of interactions of a wingtip vortex of a half-span wing and vortices generated by a slender reverse delta type add-on device were studied using Particle Image Velocimetry in a closed-loop low-speed wind tunnel. Characteristics of the vortex interactions produced downstream in planes pe...
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| Format: | Artigo |
| Język: | Inglês |
| Wydane: |
Embry-Riddle Aeronautical University
2017-09-01
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| Seria: | International Journal of Aviation, Aeronautics, and Aerospace |
| Hasła przedmiotowe: | |
| Dostęp online: | https://commons.erau.edu/ijaaa/vol4/iss3/7 |
| Etykiety: |
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