Vortex Breakdown-Edge Interaction: Consequence of Edge Oscillations

Author:

Sahin B.,Akilli H.,Lin J.-C.,Rockwell D.

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Cited by 14 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献

1. Near-surface particle image velocimetry measurements over a yawed slender delta wing;Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering;2021-03-11

2. Investigation of crossflow features of a slender delta wing;WIND STRUCT;2020

3. Dye visualization over double delta wing with various kink angles;Journal of Visualization;2019-05-02

4. The effect of angle of attack on the flow structure over the nonslender lambda wing;Aerospace Science and Technology;2013-07

5. Observation of the Vortical Flow over a Yawed Delta Wing;Journal of Aerospace Engineering;2012-10

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