Application study on plasma ignition in aeroengine strut–cavity–injector integrated afterburner
Author:
Funder
航空发动机加力燃烧室等离子体点火机理研究
燃烧室等离子体强化燃烧机理研究
Publisher
IOP Publishing
Subject
Condensed Matter Physics
Link
https://iopscience.iop.org/article/10.1088/2058-6272/ac183c/pdf
Reference40 articles.
1. Rate dependent transition to thermoacoustic instability via intermittency in a turbulent afterburner
2. Effect of non-uniform inlet profile on the combustion performance of an afterburner with bluff body
3. Instability and mode transition analysis of a hydrogen-rich combustion in a model afterburner
4. Combustion modes of hydrogen jet combustion in a cavity-based supersonic combustor
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