An experimental investigation of the near wake of a slender cone at M infinity equal 8 and 12.
Author:
Affiliation:
1. Polytechnic Institute of Brooklyn, Freeport, N. Y.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.3382
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1. Turbulent Diffusion in the Wake of a Blunt-Nosed Body at Hypersonic Speeds
2. CHEMICAL EFFECTS IN EXTERNAL HYPERSONIC FLOWS
3. Recent studies of the laminar base-flow region
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