Numerical analysis of shock-induced separation alleviation using vortex generators-Reference-Cited by-同舟云学术

Numerical analysis of shock-induced separation alleviation using vortex generators

Published:1992-01-06 Issue: Volume: Page:
ISSN:
Container-title:30th Aerospace Sciences Meeting and Exhibit
language:
Short-container-title:

Author:

MOUNTS JON¹,BARBER THOMAS¹

Affiliation:

1. United Technologies Research Center, East Hartford, CT

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1992-751

Reference22 articles.

1. Kooi, J.i\'."Influence of Free-Stream hlach Numbcr 011 'liansoiiic Sliock-\Vave Boundary Layer Iof,eraction,"XLR hIP 78013 U, %arch, 1978.

2. I'owers, \V.E. "Application of Vortex Generators for 13oundary Layer Control Through a Shock," United Aircraft Research Depart.ment Report R954;i-6,July, 1952.

3. 40 -1 0

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