Combustion Instability in Gas Rockets
Author:
Affiliation:
1. Princeton University, Princeton, N. J.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.55206
Reference4 articles.
1. An Experimental Study of High-Frequency Combustion Pressure Oscillations
2. Tsuji, H. and Takeno, T. "Studies of high frequency combustion oscillations in a gaseous propellant rocket motor/' 10th Symposium on Combustion, Cambridge Univ. Combustion Institute, pp.104-110 (1964).
3. A shock wave model of unstable rocket combustors
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