An Experimental Investigation of the Flowfield around a Yawed Cone
Author:
Affiliation:
1. U.S. Naval Ordnance Laboratory, Silver Spring, Md.
2. Naval Ordnance Systems Command, Washington, D.C.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.49918
Reference24 articles.
1. H. Supersonic Flows with Shock Waves
2. Inviscid flowfield about a pointed cone at an angle of attack.
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