Two-Dimensional Model for Liquid-Rocket Transverse Combustion Instability
Author:
Affiliation:
1. Department of Mechanical and Aerospace Engineering, University of California, Irvine, California 92697
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.J052512
Reference61 articles.
1. HarrjeD.ReardonF. “Liquid Propellant Rocket Combustion Instability,” NASA SP194, 1972.
2. Comprehensive review of liquid-propellant combustion instabilities in F-1 engines
3. High frequency combustion instability in rockets with distributed combustion
4. CroccoL.ChengS.I. “Theory of Combustion Instability in Liquid Propellant Rocket Motors,” AGARD, Monograph 8, 1956.
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