Streamwise vortex production by pitched and skewed jets in a turbulent boundary layer
Author:
Affiliation:
1. Stanford University, Stanford, California 94305
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.10967
Reference9 articles.
1. Tests of wall blowing concepts for diffuser boundary layer control
2. Vortex generator jets - Means for flow separation control
3. Investigation of several passive and active methods for turbulent flow separation control
4. INTRODUCTION TO SHOCK-INDUCED SEPARATION AND ITS PREVENTION BY DESIGN AND BOUNDARY LAYER CONTROL
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