Influence of Spike Shape at Supersonic Flow Past Blunt-Nosed Bodies: Experimental Study
Author:
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/2.1745
Reference7 articles.
1. Transonic flow modes of an axisymmetric blunt body
2. Modes of shock-wave oscillations on spike-tipped bodies
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