Hypersonic Buzz Phenomenon on the Spiked Blunt Cones
Author:
Affiliation:
1. Indian Institute of Science
2. Shock Wave Research Center
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2003-284
Reference11 articles.
1. LXVIII. Experiments on separation of boundary layers on probes in front of blunt-nosed bodies in a supersonic air stream
2. Preliminary Investigations of Spiked Bodies at Hypersonic Speeds
3. Hypersonic flow over axially symmetric spiked bodies
4. Asymmetric shock-wave oscillations on spiked bodies of revolution
5. Pulsating flows about axisymmetric concave bodies
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