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Rotating Detonation Combustion Characteristics of Kerosene-Fueled Wide-Area Scramjets

Through the method of three-dimensional numerical simulation, the rotating detonation combustion characteristics of kerosene-fueled scramjets in the range of Ma=3~7 were studied. In the flight condition of Ma=3, due to the poor effect of fuel atomization and evaporation, the detonation combustion of...

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Xehetasun bibliografikoak
Egile Nagusiak: Chen SHU, Futao GU, Bin CHEN, Chenglong YAN, Yiheng TONG, Wei LIN
Formatua: Artigo
Hizkuntza:Chinês
Argitaratua: China Astronautic Publishing CO., LTD. ; Editorial Office of Physics of Gases 2024-03-01
Saila:气体物理
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Sarrera elektronikoa:http://qtwl.xml-journal.net/cn/article/doi/10.19527/j.cnki.2096-1642.1082
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