Oscillatory Characteristics of Shallow Open Cavities in Supersonic Flow
Author:
Affiliation:
1. University of New South Wales, Canberra, Australian Capital Territory 2600, Australia
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.J054089
Reference44 articles.
1. RossiterJ. “Wind Tunnel Experiments on the Flow over Rectangular Cavities at Subsonic and Transonic Speeds,” Ministry of Aviation TR-3438, 1964.
2. TracyM.PlentovichE. “Characterization of Cavity Flow Fields Using Pressure Data Obtained in the Langley 0. 3 Meter Transonic Cryogenic Tunnel,” NASA TR-4436, 1993.
3. Flow-induced pressure oscillations in shallow cavities
4. Supersonic Cavity Flows and Their Control
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