Effects of Counterflow on the Aeroacoustic Properties of a Supersonic Jet-Reference-Cited by-同舟云学术

Effects of Counterflow on the Aeroacoustic Properties of a Supersonic Jet

Published:1999-03 Issue:2 Volume:36 Page:451-457
ISSN:0021-8669
Container-title:Journal of Aircraft
language:en
Short-container-title:Journal of Aircraft

Author:

Shih C.¹,Alvi F. S.¹,Washington D. M.¹

Affiliation:

1. Florida A&M University and Florida State University, Tallahassee, Florida 32316-2175

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/2.2451

Reference10 articles.

1. Strykowski, P. J., Krothapalli, A., and Jendoubi, S. "The Effect of Counterflow on the Development of Compressible Shear Layers/' Journal of Fluid Mechanics, Vol.308, Feb. 1996, pp.63-96.

2. 2Van der Veer, M. R. "Counterflow Thrust Vectoring of a Subsonic Rectangular Jet," M.S. Thesis, Dept. of Mechanical Engineering,Univ. of Minnesota, Minneapolis, MN,1995.

3. Counterflow thrust vectoring of supersonic jets

4. Multi-axis fluidic thrust vectoring of supersonic jets via counterflow

5. Multiaxis fluidic thrust vector control of a supersonic jet using counterflow

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