Performance analysis of dual-duct rotating detonation aero-turbine engine

标题
Performance analysis of dual-duct rotating detonation aero-turbine engine
作者
关键词
Rotating detonation aero-turbine engine, Detonation based propulsion, Thermodynamic analysis, Overall performance, Optimum compressor pressure ratios
出版物
AEROSPACE SCIENCE AND TECHNOLOGY
Volume 92, Issue -, Pages 806-819
出版商
Elsevier BV
发表日期
2019-07-09
DOI
10.1016/j.ast.2019.07.011

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