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Thermochemical non-equilibrium flow characteristics of high Mach number inlet in a wide operation range 期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2023, 卷号: 36, 期号: 12, 页码: 164-184
Authors:  Dai, Chunliang;  Sun, Bo;  Yue LJ(岳连捷);  Zhou, Shengbing;  Zhuo, Changfei;  Zhou, Changsheng;  Yu, Jianyi
Adobe PDF(5674Kb)  |  Favorite  |  View/Download：55/7  |  Submit date：2024/02/19
Scramjet inlet  Starting ability  Thermochemical  Work performance  
Numerical study of high temperature non-equilibrium effects of double-wedge in hypervelocity flow 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2022, 卷号: 124, 页码: 17
Authors:  Dai, Chunliang;  Sun, Bo;  Zhuo, Changfei;  Zhou, Shengbing;  Zhou, Changsheng;  Yue LJ(岳连捷)
Adobe PDF(6822Kb)  |  Favorite  |  View/Download：188/32  |  Submit date：2022/07/18
Hypervelocity double-wedge flow  High temperature non-equilibrium effects  Laminar and turbulence flow  Shock wave interaction  Shock wave  boundary layer interaction  
Influence of high temperature non-equilibrium effects on Mach 12 scramjet inlet 期刊论文
ACTA ASTRONAUTICA, 2022, 卷号: 193, 页码: 237-254
Authors:  Dai, Chunliang;  Sun, Bo;  Zhou, Shengbing;  Zhuo, Changfei;  Zhou, Changsheng;  Yue LJ(岳连捷)
Adobe PDF(13791Kb)  |  Favorite  |  View/Download：175/40  |  Submit date：2022/05/17
Mach 12 scramjet inlet  High temperature  Non-equilibrium effects  Thermochemical  Inlet performance  
Study of shock train/flame interaction and skin-friction reduction by hydrogen combustion in compressible boundary layer 期刊论文
INTERNATIONAL JOURNAL OF HYDROGEN ENERGY, 2020, 卷号: 45, 期号: 31, 页码: 15683-15696
Authors:  Xue R(薛瑞);  Zheng X;  Yue LJ(岳连捷);  Zhang SK;  Weng C
Adobe PDF(3251Kb)  |  Favorite  |  View/Download：358/112  |  Submit date：2020/07/06
Compressible boundary layer combustion  Skin-friction reduction  Shock train/flame interaction