Supersonic Cavity Flow Control Using a Spanwise Array of Leading-Edge Tabs-Reference-Cited by-同舟云学术

Supersonic Cavity Flow Control Using a Spanwise Array of Leading-Edge Tabs

Published:2022-05 Issue:3 Volume:59 Page:788-798
ISSN:1533-3868
Container-title:Journal of Aircraft
language:en
Short-container-title:Journal of Aircraft

Author:

Singh Surabhi,Ukeiley Lawrence,Zhang Yang^ORCID,Cattafesta Louis,Taira Kunihiko¹

Affiliation:

1. University of California, Los Angeles, California 90095

Funder

Air Force Office of Scientific Research

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/1.C036678

Reference52 articles.

1. RoshkoA. “Some Measurements of Flow in a Rectangular Cutout,” NACA TN 3488, 1955.

2. KrishnamurtyK. “Acoustic Radiation from Two-Dimensional Rectangular Cutouts in Aerodynamic Surfaces,” NACA TN 3487, 1955.

3. RossiterJ. “Wind Tunnel Experiments on the Flow over Rectangular Cavities at Subsonic and Transonic Speeds,” Aeronautical Research Council, Ministry of Aviation TR 3438, 1964.

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

5. Review—Self-Sustaining Oscillations of Flow Past Cavities

Cited by 6 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. Effects of doors on an open cavity flow at Mach number 6;Chinese Journal of Aeronautics;2024-08

2. Experimental Investigation on the Flow-Induced Oscillation in Deep Cavity and the Controlling Effect Using Wedge Spoiler;Lecture Notes in Mechanical Engineering;2024

3. Experimental Investigation of Control Effects of Flapping Jets on Supersonic Cavity Flow;AIAA Journal;2023-12-29

4. The effect of an internal object on self-sustained oscillations in a flow past a louvered cavity;Physics of Fluids;2023-11-01

5. Experimental investigation of the supersonic cavity by spectral-POD of high-sampling rate pressure-sensitive paint data;Experiments in Fluids;2023-05