Supersonic Flow over a Deep Cavity for a Laser Application-Reference-Cited by-同舟云学术

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Supersonic Flow over a Deep Cavity for a Laser Application

Published:1979-02 Issue:2 Volume:17 Page:216-219
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Shen Peter¹

Affiliation:

1. Northrop Corporation, Hawthorne, Calif.

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/3.61099

Reference5 articles.

1. An Investigation of Separated Flows - Part I: The Pressure Field

2. 2Petty, J., Private communication; Petty,J., Cooper, J., Kordegi, R., and Ortwerth, P.J. "The Use of Shaped Cavities to Improve the Side Wall Boundary Layer Quality in Gas Dynamic Lasers," Laser Digest, Fall1974, AFWL-TR-74-344, pp.202-230.

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1. Shock and shear layer interactions in a confined supersonic cavity flow;Physics of Fluids;2021-06

2. Supersonic Flow over a Finite-Width Rectangular Cavity;AIAA Journal;2015-02

3. Supersonic Flow over a Finite-Width Rectangular Cavity;51st AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition;2013-01-05

4. Particle Image Velocimetry of a Three-Dimensional Supersonic Cavity Flow;50th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition;2012-01-09

5. Effect of Upstream Mass-Injection on Cavity Flow Oscillations ( PIV Measurements Compared with CFD Predictions);41st Aerospace Sciences Meeting and Exhibit;2003-01-06

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