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...
Tallennettuna:
| Päätekijä: | |
|---|---|
| Aineistotyyppi: | Artigo |
| Kieli: | Inglês |
| Julkaistu: |
Embry-Riddle Aeronautical University
2017-09-01
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| Sarja: | International Journal of Aviation, Aeronautics, and Aerospace |
| Aiheet: | |
| Linkit: | https://commons.erau.edu/ijaaa/vol4/iss3/7 |
| Tagit: |
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