HEAT TRANSFER TO A HEMISPHERE-CYLINDER AT LOW REYNOLDS NUMBERS
Author:
Affiliation:
1. University of California, Berkeley, Calif.
2. Heliodyne Corporation, Westwood, Calif.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.1610
Reference20 articles.
1. Shock Wave and Flow Field Development in Hypersonic Re-Entry
2. Ho, H. T. and Probstein, R. F., Rarefied Gas Dynamics (Academic Press, New York, 1961), pp.525-552.
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