Optical Diagnostics for Characterizing a Transitional Shear Layer over a Supersonic Cavity-Reference-Cited by-同舟云学术

Optical Diagnostics for Characterizing a Transitional Shear Layer over a Supersonic Cavity

Published:2013-12 Issue:12 Volume:51 Page:2977-2982
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Hargather Michael J.¹,Settles Gary S.¹,Gogineni Sivaram²

Affiliation:

1. Mechanical Engineering Department, Pennsylvania State University, University Park, Pennsylvania 16802

2. Spectral Energies, LLC, Dayton, Ohio 45431

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.J052421

Reference19 articles.

1. RossiterJ. E. “Wind-Tunnel Experiments on the Flow over Rectangular Cavities at Subsonic and Transonic Speeds,” Aeronautical Research Council, Rept. and Memoranda No.3438, London, Oct. 1964.

2. Experiments on compressible flow-induced cavity oscillations

3. Time resolved flow-field measurements of a turbulent mixing layer over a rectangular cavity

4. Supersonic Cavity Flows and Their Control

5. Performance Results for the Optical Turbulence Reduction Cavity

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