Nonlinear Combustion Instability in a Multi-Injector Rocket Engine-Reference-Cited by-同舟云学术

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Nonlinear Combustion Instability in a Multi-Injector Rocket Engine

Published:2020-01 Issue:1 Volume:58 Page:219-235
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Xiong Juntao¹,Morgan Hugh¹,Krieg Jeremy¹,Liu Feng¹,Sirignano William A.¹

Affiliation:

1. University of California, Irvine, Irvine, California 92697

Funder

Air Force Office of Scientific Research

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

https://arc.aiaa.org/doi/am-pdf/10.2514/1.J058036

Reference26 articles.

1. PoinsotT.VeynanteD., Theoretical and Numerical Combustion, 3rd ed., Aquaprint, Bordeaux, France, 2011, pp. 391–393.

2. HarrjeD.ReardonF. “Liquid Propellant Rocket Combustion Instability,” NASA SP 194, 1972.

3. Comprehensive review of liquid-propellant combustion instabilities in F-1 engines

4. CroccoL.ChengS. L. “Theory of Combustion Instability in Liquid Propellant Rocket Motors,” AGARD Monograph 8, Neuilly-Sur-Seine, France, 1956.

5. A shock wave model of unstable rocket combustors

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