Mixing of a Sonic Transverse Jet Injected into a Supersonic Flow-Reference-Cited by-同舟云学术

Mixing of a Sonic Transverse Jet Injected into a Supersonic Flow

Published:2000-03 Issue:3 Volume:38 Page:470-479
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

VanLerberghe Wayne M.¹,Santiago Juan G.²,Dutton J. Craig³,Lucht Robert P.⁴

Affiliation:

1. The Aerospace Corporation, El Segundo, California 90245

2. Stanford University, Stanford, California 94305

3. University of Illinois at Urbana–Champaign, Urbana, Illinois 61801

4. Texas A&M University, College Station, Texas 77843

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/2.984

Reference14 articles.

1. 1Gruber, M. R. “An Experimental Investigation of Transverse Injection from Circular and Elliptical Nozzles into a Supersonic Crossflow,” Ph.D. Dissertation, Dept. of Mechanical and Industrial Engineering,Univ. of Illinois, Urbana, IL,Jan. 1996.

2. Characteristic features of large structures in compressible mixing layers

3. Large-scale structure and entrainment in the supersonic mixing layer

4. On density effects and large structure in turbulent mixing layers

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