Influences of propeller advance ratio on delta-winged uav model vortex properties
The flow above the upper surface of delta wing is dominated by a very complicated and unresolved vortex structure. This study investigates the effects of the propeller advance ratio on the vortex properties and vortex breakdown above a generic 55° sharp-edged non-slender delta wing UAV model. The ex...
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| Main Authors: | , , , , , , , , |
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| Format: | Article |
| Published: |
The Aeronautical and Astronautical Society of the Republic of China
2019
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| Subjects: | |
| Online Access: | http://eprints.utm.my/id/eprint/88554/ http://dx.doi.org/10.6125/JoAAA.201906_51(2).04 |
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