Buzz Cycle Description in an Axisymmetric Mixed-Compression Air Intake
Author:
Affiliation:
1. Sharif University of Technology, 145888 Tehran, Iran
2. Ferdowsi University of Mashhad, 91779 Mashhad, Iran
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.J054215
Reference47 articles.
1. OswatitschK. “Pressure Recovery in Missile in Reaction Propulsion at High Supersonic Speeds,” NACA TM-1140, 1947.
2. Analysis of self-excited oscillations in fluid flows
3. FerriA.NucciL. M. “The Origin of Aerodynamic Instability of Supersonic Inlet at Subcritical Condition,” NACA RM-L50K30, 1951.
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