Effects of Transition Reynolds Number on Empirical Constants of the Rossiter Formula
Author:
Affiliation:
1. Gyeongsang National University, Jinju 52828, Republic of Korea
Funder
National Research Foundation of Korea
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.J063454
Reference27 articles.
1. Cavity Oscillation Mechanisms in High-Speed Flows
2. Interaction between feedback aeroacoustic and acoustic resonance mechanisms in a cavity flow: a global stability analysis
3. Mechanism of sound generation by low Mach number flow over a wall cavity
4. RossiterJ. “Wind-Tunnel Experiments on the Flow over Rectangular Cavities at Subsonic and Transonic Speeds,” RAE TR 64037, London, 1964.
5. Flow-induced pressure oscillations in shallow cavities
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