Theoretical Investigation of the Flow Field About Blunt-Nosed Bodies in Supersonic Flight
Author:
Affiliation:
1. Polytechnic Institute of Brooklyn and Gruen Applied Science Laboratories, Inc.,
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Link
http://arc.aiaa.org/doi/pdf/10.2514/8.7883
Reference12 articles.
1. Supersonic flow past a bluff body with a detached shock Part I Two-dimensional body
2. Vaglio-Llaurin, R., Supersonic Flow-Field About Blunt-Nosed Bodies of Revolution-Part S-The Methods of Analysis for the Subsonic and Sonic Regions, Gruen Applied Science Labs., Tech. Rep. No. 4,October, 1956.
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