Transonic Shockwave/Turbulent-Boundary-Layer Interaction with Suction or Blowing
Author:
Affiliation:
1. Virginia Polytechnic Institute and State University, Blacksburg, Va.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.58442
Reference32 articles.
1. INTRODUCTION TO SHOCK-INDUCED SEPARATION AND ITS PREVENTION BY DESIGN AND BOUNDARY LAYER CONTROL
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