Base Flow of Circular Cylinder at Hypersonic Speeds
Author:
Affiliation:
1. University of New South Wales, Canberra, Australian Capital Territory 2600, Australia
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.J054270
Reference42 articles.
1. AndersonJ. D., Hypersonic and High Temperature Gas Dynamics, McGraw–Hill, New York, 1989, pp. 363–652.
2. Initiation and development of separated flow behind a circular cylinder in a supersonic stream
3. Near wake of a hypersonic blunt body with mass addition
4. Near wake of a blunt body at hypersonic speeds
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