Reduction of fluctuating pressure loads in shock/boundary-layer interactions using vortex generators
Author:
Affiliation:
1. University of Texas at Austin, Austin, Texas 78712
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.12736
Reference24 articles.
1. Experimental investigation of effect of tangential blowing and wall cooling on flow with separation
2. Injection slot location for boundary-layer control in shock-induced separation
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