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Experimental Study of Longitudinal Stage Separation of Two-Body Configuration in Shock Tunnel 期刊论文
AIAA Journal, 2022, 卷号: 60, 期号: 12, 页码: 6940-6946
作者:  Wang Y(王粤);  Wang YP(汪运鹏);  Jiang ZL(姜宗林)
Adobe PDF(2434Kb)  |  收藏  |  浏览/下载：306/81  |  提交时间：2022/08/23
Aerodynamic Coefficients  Two Stage to Orbit  Aerodynamic Performance  Hypersonic Flight  Hypersonic Wind Tunnels  Solenoid Valves  Oblique Shock  Pneumatic Actuator  Hypersonic Flows  Computer Aided Engineering  
Stabilization Mechanism of Burner-attached Flames in Laminar Non-premixed Jets 期刊论文
COMBUSTION SCIENCE AND TECHNOLOGY, 2022, 卷号: 194, 期号: 14, 页码: 21
作者:  Li D(李丹);  Liu Yu Cheng;  Wang SF(王双峰)
Adobe PDF(10115Kb)  |  收藏  |  浏览/下载：250/60  |  提交时间：2021/05/17
Burner-attached flame  laminar non-premixed jets  flame stabilization  conductive heat transfer  convective heat transfer  
A single-camera synthetic Schlieren method for the measurement of free liquid surfaces 期刊论文
EXPERIMENTS IN FLUIDS, 2021, 卷号: 62, 期号: 11, 页码: 15
作者:  Li, Huixin;  Avila, Marc;  Xu D(徐多)
Adobe PDF(7496Kb)  |  收藏  |  浏览/下载：232/65  |  提交时间：2021/11/15
Experimental study on shock wave control in high-enthalpy hypersonic flow by using SparkJet actuator 期刊论文
ACTA ASTRONAUTICA, 2021, 卷号: 188, 页码: 416-425
作者:  Xie, Wei;  Luo, Zhenbing;  Zhou, Yan;  Gao, Tianxiang;  Wu, Yun;  Wang Q(汪球)
Adobe PDF(8485Kb)  |  收藏  |  浏览/下载：116/58  |  提交时间：2022/10/25
SparkJet  High-enthalpy hypersonic flow  Shock control  Shock-on-shock interaction  Air supply  
Hysteresis of Shock Train Movement in the Isolator with a Ramp 期刊论文
AIAA JOURNAL, 2021, 卷号: 59, 期号: 10, 页码: 3873-3882
作者:  Huang TL(黄庭隆);  Zhang QF(张启帆);  Yue LJ(岳连捷);  Zhang P;  Zhao QJ
Adobe PDF(2961Kb)  |  收藏  |  浏览/下载：204/42  |  提交时间：2022/02/17
Reconstructing shock front of unstable detonations based on multi-layer perceptron 期刊论文
ACTA MECHANICA SINICA, 2021, 页码: 14
作者:  Zhou, Lin;  Teng, Honghui;  Ng, Hoi Dick;  Yang PF(杨鹏飞);  Jiang ZL(姜宗林)
Adobe PDF(6382Kb)  |  收藏  |  浏览/下载：218/32  |  提交时间：2021/11/01
Cellular detonation  Lead shock evolution  Multi-layer perceptron  Numerical simulations  
Theoretical, numerical and experimental study of hypersonic boundary layer transition: Blunt circular cone 期刊论文
APPLIED THERMAL ENGINEERING, 2021, 卷号: 194, 页码: 14
作者:  Chen, Jianqiang;  Yi, Shihe;  Li XL(李新亮);  Han GL(韩桂来);  Zhang, Yifeng;  Yang, Qiang;  Yuan, Xianxu
Adobe PDF(11175Kb)  |  收藏  |  浏览/下载：317/89  |  提交时间：2021/08/03
Hypersonic boundary layer  Stability  Transition  Thermal protection  
Effects of slope and speed of escalator on the dispersion of cough-generated droplets from a passenger 期刊论文
PHYSICS OF FLUIDS, 2021, 卷号: 33, 期号: 4, 页码: 7
作者:  Li ZB(李曌斌);  Zhang XL(张鑫磊);  Wu T(吴霆);  Zhu LX(朱力行);  Qin JH(秦建华);  Yang XL(杨晓雷)
Adobe PDF(4107Kb)  |  收藏  |  浏览/下载：185/37  |  提交时间：2021/05/17
Direct numerical simulation of a supersonic turbulent boundary layer over a compression–decompression corner 期刊论文
Physics of Fluids, 2021, 卷号: 33, 页码: 065111
作者:  段俊亦;  李欣;  李新亮;  刘洪伟
Adobe PDF(5069Kb)  |  收藏  |  浏览/下载：170/42  |  提交时间：2021/11/23
Advances in critical technologies for hypersonic and high-enthalpy wind tunnel 期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2020, 卷号: 33, 期号: 12, 页码: 3027-3038
作者:  Jiang ZL(姜宗林);  Hu ZM(胡宗民);  Wang YP(汪运鹏);  Han GL(韩桂来)
Adobe PDF(1129Kb)  |  收藏  |  浏览/下载：321/168  |  提交时间：2021/03/30
High-enthalpy flow  Hypersonic wind tunnel  Aerospace vehicle  Aerodynamic balance  Heat flux sensor  Optical measurement technique