Inviscid flowfield about a pointed cone at an angle of attack.
Author:
Affiliation:
1. General Applied Science Laboratories Inc., Westbury, N. Y.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.4064
Reference9 articles.
1. Supersonic flow past cones of general cross-section
2. A time-dependent computational method for blunt body flows.
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