Asymmetric shock-wave oscillations on spiked bodies of revolution
Author:
Affiliation:
1. Aeronutronic Ford Corporation, Newport Beach, Calif.
2. USAF/SAMSO, El Segundo, Calif.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/3.27945
Reference5 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. Hypersonic flow over spiked cones
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