Edge tones in high-speed flows and their application to multiple-jetmixing-Reference-Cited by-同舟云学术

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Edge tones in high-speed flows and their application to multiple-jetmixing

Published:1983-07 Issue:7 Volume:21 Page:937-938
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Krothapalli A.¹,Karamcheti K.¹,Hsia Y.¹,Baganoff D.¹

Affiliation:

1. Joint Institute for Aeronautics and Acoustics, Stanford University, Stanford, California

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/3.8180

Reference3 articles.

1. Karamcheti, K., Bauer, A., Shields, W.L., Stegen, G., and Woolley, P.J. "Some Features of an Edge Tone Flow Field/' NASA SP-207, 1969.

2. Woolley, P.J. "An Investigation of Edge Tones and the Role of Flow Field Instability in their Generation," Ph.D. Thesis,Stanford University, Stanford, Calif. 1973.

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1. Discrete tones in subsonic jet engine test cells;Progress in Aerospace Sciences;2018-08

2. Experimental and Theoretical Investigations of Edge Tones in High Speed Jets;Journal of Fluid Science and Technology;2013

3. Computational Analysis of Mach Number Effects on the Edgetone Phenomenon;AIAA Journal;2010-06

4. A review of jet mixing enhancement for aircraft propulsion applications;Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering;2006-02-01

5. Structure of Supersonic Twin Jets;AIAA Journal;2005-11

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