Some experiments in the near wake of cones.
Author:
Affiliation:
1. Aeronutronic Division of Philco-Ford Corporation, Newport Beach, Calif.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.4202
Reference9 articles.
1. Direct measurement of velocity by hot-wire anemometry
2. Dewey, C. F., Jr. "The near wake of a blunt body at hypersonic speeds/' AIAA Paper 64-43 (1964).
3. Base pressure measurements on sharp and blunt 9 deg cones at Mach numbers from 3.50 to 9.20.
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4. Experimental Study of Supersonic Laminar Base Flow with and without Suction;AIAA Journal;1973-12
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