Effect of a spike on the drag and on the aerodynamic stability of blunt bodies in supersonic flow
Author:
Affiliation:
1. Technion—Israel Institute of Technology, Haifa, Israel
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/3.30094
Reference16 articles.
1. LXVIII. Experiments on separation of boundary layers on probes in front of blunt-nosed bodies in a supersonic air stream
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