Numerical simulation on the combustion characteristics of scramjet at high Mach number

Numerical simulation on the combustion characteristics of scramjet at high Mach number

To investigate the problem of ethylene jet mixing and combustion in the scramjet at high Mach number (Ma = 8), numerical simulations were carried out for different equivalent ratios at cold and combustion conditions, in which three-dimensional steady compressible RANS and k-ω SST turbulence model we...

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Bibliographic Details
Main Authors: Jiahang Li, Zhaoyang Xia, Mi Yan, Hao Zhang, Jinfeng Dang, Majie Zhao
Format: Article
Language:English
Published: KeAi Communications Co., Ltd. 2025-08-01
Series:Defence Technology
Subjects:
Scramjet
High Mach number
Equivalence ratio
Combustion mode
Flame structure
Online Access:http://www.sciencedirect.com/science/article/pii/S2214914725001345
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