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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:162/25  |  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  
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:332/115  |  提交时间:2020/03/21
Hysteresis  Dual-mode scramjet  Supersonic combustion  Mode transition  Flame stabilization  Combustion oscillation  
A theoretical and computational study of the vibration excitation on the transition criteria of shock wave reflections 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2019, 卷号: 89, 页码: 299-306
作者:  Peng J(彭俊);  Zhang ZJ(张子健);  Hu ZM(胡宗民);  Jiang ZL(姜宗林)
浏览  |  Adobe PDF(2165Kb)  |  收藏  |  浏览/下载:399/93  |  提交时间:2019/09/09
Shock reflection  Vibration excitation  Mach reflection  Transition criterion  Hypersonic flow