Publisher
American Institute of Aeronautics and Astronautics
Reference32 articles.
1. 1Rossiter, J. “Wind Tunnel Experiments on the Flow Over Rectangular Cavities at Subsonic and Transonic Speeds,” Tech. Rep. 64037, Royal Aircraft Establishment, October 1964.
2. On the tones and pressure oscillations induced by flow over rectangular cavities
3. Compressible cavity flow oscillation due to shear layer instabilities and pressure feedback
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