Analysis of spontaneous longitudinal combustion instability in an O2/CH4 single-injector rocket combustor
Author:
Funder
Foundation for Innovative Research Groups of the National Natural Science Foundation of China
Publisher
Elsevier BV
Subject
Aerospace Engineering
Reference47 articles.
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4. Injector-driven combustion instabilities in a hydrogen/oxygen rocket combustor;Gröning;J. Propuls. Power,2016
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