Investigation of Cavity Flow Using Fast-Response Pressure-Sensitive Paint-Reference-Cited by-同舟云学术

Investigation of Cavity Flow Using Fast-Response Pressure-Sensitive Paint

Published:2014-11 Issue:11 Volume:52 Page:2462-2470
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Flaherty W.¹,Reedy Todd M.¹,Elliott Gregory S.¹,Austin J. M.¹,Schmit Ryan F.²,Crafton J.³

Affiliation:

1. Department of Aerospace Engineering, University of Illinois at Urbana–Champaign, Champaign, Illinois 61801

2. U.S. Air Force Research Laboratory, Wright–Patterson Air Force Base, Ohio 45433

3. Innovative Scientific Solutions, Inc., Dayton, Ohio 45440

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.J052864

Reference30 articles.

1. RossiterJ. E. “Wind-Tunnel Experiments on the Flow over Rectangular Cavities at Subsonic and Transonic Speeds,” Ministry of Aviation and Memoranda, Rept. 3438, London, 1966.

2. Characteristics of the Compressible Shear Layer over a Cavity

3. HellerH.BlissD. “Aerodynamically Induced Pressure Oscillations in Cavities- Physical Mechanisms and Suppression Concepts,” AFFDL TR-74-133, 1974.

4. On the tones and pressure oscillations induced by flow over rectangular cavities

5. Supersonic Cavity Flows and Their Control

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