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Direct numerical simulation of slender cones with variable nose bluntness based on graphics processing unit computation 期刊论文
PHYSICS OF FLUIDS, 2023, 卷号: 35, 期号: 7, 页码: 74112
Authors:  Zhu YH(朱艳华);  Li XL(李新亮);  Guo TB(郭同彪);  Liu HW(刘洪伟);  Tong FL(童福林)
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Numerical Investigation on Longitudinal Stage Separation of Spiked Two-Stage-to-Orbit Vehicle 期刊论文
Journal of Spacecraft and Rockets, 2023, 卷号: 60, 期号: 1, 页码: 215-229
Authors:  Wang Y(王粤);  Wang YP(汪运鹏);  Wang C(王春);  Jiang ZL(姜宗林)
Adobe PDF(5479Kb)  |  Favorite  |  View/Download：431/82  |  Submit date：2022/08/24
Multistage Launch Vehicle  Aerodynamic Characteristics  Shock Wave Interaction  Angle of Attack  Waverider  Boundary Layer Flow  Total Variation Diminishing  Adverse Pressure Gradient  Hypersonic Flows  Hypersonic Wind Tunnels  
Experimental study on the effects of the cone nose-tip bluntness 期刊论文
PHYSICS OF FLUIDS, 2022, 卷号: 34, 期号: 10, 页码: 7
Authors:  Liu MK(刘美宽);  Han GL(韩桂来);  Li, Zongxian;  Jiang ZL(姜宗林)
Adobe PDF(2020Kb)  |  Favorite  |  View/Download：206/65  |  Submit date：2022/12/29
Design of a milli-newton force balance for hypersonic rarefied wind tunnel 期刊论文
MEASUREMENT, 2021, 卷号: 185, 页码: 7
Authors:  Wu CW(吴臣武);  Liu C(刘聪);  Hu DL(胡灯亮);  Liu HL(刘宏立);  Huang HJ(黄河激)
Adobe PDF(4178Kb)  |  Favorite  |  View/Download：324/80  |  Submit date：2021/11/15
Strain  Balance  Milli-newton  Design  Calibration  
Advances in plasma-assisted ignition and combustion for combustors of aerospace engines 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2021, 卷号: 117, 页码: 27
Authors:  Li, Mengzhe;  Wang, Zhikai;  Xu, Rongguang;  Zhang, Xiaoliang;  Chen, Zhitong;  Wang Q(汪球)
Adobe PDF(8841Kb)  |  Favorite  |  View/Download：291/109  |  Submit date：2021/11/01
Non-equilibrium plasma  Plasma-assisted ignition  Plasma-assisted combustion  Aerospace engine  Combustor  Extreme condition  
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
Authors:  Huang TL(黄庭隆);  Zhang QF(张启帆);  Yue LJ(岳连捷);  Zhang P;  Zhao QJ
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Performance analysis of a strut-aided hypersonic scramjet by full-scale IDDES modeling 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2021, 卷号: 117, 页码: 14
Authors:  Yao W(姚卫);  Liu H(刘杭);  Yue LJ(岳连捷);  Xiao YB(肖雅彬)
Adobe PDF(2954Kb)  |  Favorite  |  View/Download：299/72  |  Submit date：2021/11/15
Hypersonic combustion  Hydrogen  Improved Delayed Detached Eddy  Simulation (IDDES)  Dynamic zone flamelet model  Scramjet  
Numerical simulation of the effects of protrusion on DC arc anode attachment 期刊论文
Plasma Science and Technology, 2021, 卷号: 23, 期号: 10, 页码: 11
Authors:  Niu C(牛聪);  Meng X(孟显);  Huang HJ(黄河激);  ZHU,Tao;  SUN,Surong;  WANG,Haixing
Adobe PDF(1948Kb)  |  Favorite  |  View/Download：277/70  |  Submit date：2021/11/01
DC arc  arc anode attachment  anode protrusion  chemical non-equilibrium  
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
Authors:  Chen, Jianqiang;  Yi, Shihe;  Li XL(李新亮);  Han GL(韩桂来);  Zhang, Yifeng;  Yang, Qiang;  Yuan, Xianxu
Adobe PDF(11175Kb)  |  Favorite  |  View/Download：358/101  |  Submit date：2021/08/03
Hypersonic boundary layer  Stability  Transition  Thermal protection  
Effects of Cowl-Induced Expansion on the Wave Complex Induced by Oblique Detonation Wave Reflection 期刊论文
PROCESSES, 2021, 卷号: 9, 期号: 7, 页码: 10
Authors:  Wang, Aifeng;  Shang JH(尚佳豪);  Wang Q(汪球);  Wang KL(王宽亮)
Adobe PDF(3951Kb)  |  Favorite  |  View/Download：218/38  |  Submit date：2021/08/16
oblique detonation  asymmetric  nozzle  reflection