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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
作者:  Dai, Chunliang;  Sun, Bo;  Zhuo, Changfei;  Zhou, Shengbing;  Zhou, Changsheng;  Yue LJ(岳连捷)
Adobe PDF(6822Kb)  |  收藏  |  浏览/下载：164/26  |  提交时间：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
作者:  Dai, Chunliang;  Sun, Bo;  Zhou, Shengbing;  Zhuo, Changfei;  Zhou, Changsheng;  Yue LJ(岳连捷)
Adobe PDF(13791Kb)  |  收藏  |  浏览/下载：162/36  |  提交时间：2022/05/17
Mach 12 scramjet inlet  High temperature  Non-equilibrium effects  Thermochemical  Inlet performance  
Numerical investigation of mode transition and hysteresis in a cavity-based dual-mode scramjet combustor 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2019, 卷号: 94, 页码: 10
作者:  Zhang X(张旭);  Yue LJ(岳连捷);  Huang TL(黄庭隆);  Zhang QF(张启帆);  Zhang XY(张新宇)
浏览  |  Adobe PDF(3862Kb)  |  收藏  |  浏览/下载：334/117  |  提交时间：2020/03/21
Hysteresis  Dual-mode scramjet  Supersonic combustion  Mode transition  Flame stabilization  Combustion oscillation  
Iso-contraction-ratio methodology for the design of hypersonic inward turning inlets with shape transition 会议论文
18th AIAA/3AF International Space Planes and Hypersonic Systems and Technologies Conference 2012, Tours, France, SEP 24-28, 2012
作者:  Xiao YB(肖雅彬);  Yue LJ(岳连捷);  Chen LH(陈立红);  Zhang XY(张新宇);  Xiao YB(肖雅彬)
Adobe PDF(1674Kb)  |  收藏  |  浏览/下载：433/114  |  提交时间：2014/02/24