Spontaneous and Triggered Longitudinal Combustion Instability in a Single-Injector Liquid-Rocket Combustor
Author:
Affiliation:
1. University of California, 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.J057743
Reference40 articles.
1. CulickF. E. “Unsteady Motions in Combustion Chambers for Propulsion Systems,” AGARDograph, AG-AVT-039, Neuilly-Sur-Seine, France, 2006.
2. Two-Dimensional Model for Liquid-Rocket Transverse Combustion Instability
3. Combustion Instability with a Single-Element Swirl Injector
4. Combustion Instability of Gaseous Fuels in a Continuously Variable Resonance Chamber (CVRC)
5. Experimental Study of High-Frequency Combustion Instability in a Continuously Variable Resonance Combustor (CVRC)
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