Reduced Order Modeling Approach to Combustion Instabilities of Liquid Rocket Engines
Author:
Affiliation:
1. CNRS, CentraleSupélec, University of Paris-Saclay, 91192 Gif-sur-Yvette cedex, France
2. SAFRAN Aircraft Engines, 77550 Moissy-Cramayel, France
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.J057098
Reference65 articles.
1. Aspects of Combustion Stability in Liquid Propellant Rocket Motors Part I: Fundamentals. Low Frequency Instability With Monopropellants
2. Servo-Stabilization of Combustion in Rocket Motors
3. Comprehensive review of liquid-propellant combustion instabilities in F-1 engines
4. Thermophysical characteristics of shear-coaxial LOX–H2 flames at supercritical pressure
5. Dynamics of a transcritical coaxial flame under a high-frequency transverse acoustic forcing: Influence of the modulation frequency on the flame response
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