Role of Trailing-Edge Geometry in Open Cavity Flow Control-Reference-Cited by-同舟云学术

Role of Trailing-Edge Geometry in Open Cavity Flow Control

Published:2019-02 Issue:2 Volume:57 Page:876-878
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Liu Q.¹,Gómez F.²

Affiliation:

1. Florida State University, Tallahassee, Florida 32310

2. Aerospace Engineering and Aviation, School of Engineering, RMIT University, VIC 3083, Australia

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/1.J056977

Reference15 articles.

1. RossiterJ. “Wind-Tunnel Experiments on the Flow over Rectangular Cavities at Subsonic and Transonic Speeds,” Aeronautical Research Council Reports and Memoranda, Vol. 3438, Ministry of Aviation, Royal Aircraft Establishment, RAE Farnborough, 1964.

2. On self-sustained oscillations in two-dimensional compressible flow over rectangular cavities

3. Experimental Investigation of Oscillations in Flows Over Shallow Cavities

4. The physical mechanism of flow-induced pressure fluctuations in cavities and concepts for their suppression

5. Influence of impingement edge geometry on cavity flow oscillations

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