Inlet Buzz and Combustion Oscillation in an Axisymmetric Ramjet Engine-Reference-Cited by-同舟云学术

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Inlet Buzz and Combustion Oscillation in an Axisymmetric Ramjet Engine

Published:2010-01-04 Issue: Volume: Page:
ISSN:
Container-title:48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition
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Author:

Sung Hong-Gye¹,Yeom Hyo-won¹,Yang Vigor²,Kim Sung-Jin¹

Affiliation:

1. Korea Aerospace University

2. Georgia Institute of Technology

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2010-756

Reference27 articles.

1. 1Oswaititsch, K. "Pressure Recovery for Missiles with Reaction Propulsion at High Supersonic Speeds," NACA TM-1140, Jun.1947.

2. 2Ferri, A. and Nucci, R.M. "The Origin of Aerodynamic Instability of Supersonic Inlets at Subcritical Conditions," NACA RM-L50K30,Jan.1951.

3. 5Mirels,H."AcousticAnalysisofRam-JetBuzz,"NACATM,N0.3574-1140,1955.

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