Oscillatory Characteristics of Shallow Open Cavities in Supersonic Flow-Reference-Cited by-同舟云学术

Oscillatory Characteristics of Shallow Open Cavities in Supersonic Flow

Published:2016-11 Issue:11 Volume:54 Page:3495-3508
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Sridhar V.¹,Gai S. L.¹,Kleine H.¹

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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