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Numerical Study on the Aerodynamic Heating Characteristics of the Cantilevered Injection System for Oblique Detonation Engine Inlets 期刊论文
AEROSPACE, 2023, 卷号: 10, 期号: 10, 页码: 18
Authors:  Yang F(杨帆);  Lin MY(林明月);  Hu ZM(胡宗民);  Han GL(韩桂来)
Adobe PDF(8946Kb)  |  Favorite  |  View/Download：89/5  |  Submit date：2023/11/28
oblique detonation engine  cantilevered injection  localized high heat flux  boundary layer separation  reattachment  
Spray combustion characteristics of a gas-liquid pintle injector with variable swirl intensities 期刊论文
PHYSICS OF FLUIDS, 2023, 卷号: 35, 期号: 9, 页码: 15
Authors:  He CM(何成明);  Luo WH(罗苇航);  Zhang, Peng;  He, Zhixia;  Yue LJ(岳连捷)
Adobe PDF(6498Kb)  |  Favorite  |  View/Download：110/3  |  Submit date：2023/10/30
Hypergolic ignition induced by head on collision of bi propellant droplets: Monoethanolamine based fuel and hydrogen peroxide 期刊论文
FUEL, 2023, 卷号: 342, 页码: 127788
Authors:  Zhang DW(张大尉);  Yu DH(于德海);  Yuan YM(袁越明);  Zhang, Peng;  Fan XJ(范学军)
Adobe PDF(8756Kb)  |  Favorite  |  View/Download：242/7  |  Submit date：2023/04/20
Hypergolic Ignition  Droplet collision  Droplet swelling  Monoethanolamine  Hydrogen peroxide  
Analysis of spray characteristics of a jet film injection element based on Voronoi tessellation 期刊论文
ACTA ASTRONAUTICA, 2023, 卷号: 206, 页码: 100-113
Authors:  He CM(何成明);  Zhang, Peng;  He, Zhixia;  Yue LJ(岳连捷)
Adobe PDF(20952Kb)  |  Favorite  |  View/Download：53/4  |  Submit date：2023/04/20
Liquid rocket engine  Pintle injector  Spray characteristics  Jet film injection  Voronoi tessellation  
Transitional criterion and hysteresis of multiple shock-shock interference 期刊论文
PHYSICS OF FLUIDS, 2023, 卷号: 35, 期号: 4, 页码: 46110
Authors:  Lin MY(林明月);  Yang F(杨帆);  Hu ZM(胡宗民);  Wang C(王春);  Jiang ZL(姜宗林)
Adobe PDF(5430Kb)  |  Favorite  |  View/Download：88/7  |  Submit date：2023/06/15
Transitional wave configurations between Type III and Type IV oblique shock/bow shock interactions 期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2023, 卷号: 36, 期号: 3, 页码: 96-106
Authors:  Peng J(彭俊);  Li S(李帅);  Yang F(杨帆);  Lin MY(林明月);  Han GL(韩桂来);  Hu ZM(胡宗民)
Adobe PDF(2838Kb)  |  Favorite  |  View/Download：63/3  |  Submit date：2023/04/20
Shock interactions  Transitional configuration  Aerodynamic heating  Shear layer  Mach interaction  
Experimental study of the spray characteristics of twin-fluid atomization: Focusing on the annular flow regime 期刊论文
PHYSICS OF FLUIDS, 2022, 卷号: 34, 期号: 12, 页码: 21
Authors:  Liu C(刘畅);  Wu K(吴坤);  Zhang, Zhenyu;  Yuan YM(袁越明);  Fan XJ(范学军)
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Lagrange Optimization of Shock Waves for Two-Dimensional Hypersonic Inlet with Geometric Constraints 期刊论文
AEROSPACE, 2022, 卷号: 9, 期号: 10, 页码: 15
Authors:  Li YL(李育凌);  Yue LJ(岳连捷);  He CM(何成明);  Wu WN(邬婉楠);  Chen H(陈昊)
Adobe PDF(3520Kb)  |  Favorite  |  View/Download：260/80  |  Submit date：2022/11/14
scramjet inlet  Lagrange optimization method  shock configuration  
Spin-affected reflexive and stretching separation of off-center droplet collision 期刊论文
PHYSICAL REVIEW FLUIDS, 2022, 卷号: 7, 期号: 1, 页码: 25
Authors:  He CM(何成明);  Yue LJ(岳连捷);  Zhang,Peng
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Experimental study of mode transition characteristics of a cavity-based scramjet combustor during acceleration 期刊论文
Aerospace Science and Technology, 2019, 卷号: 93, 期号: 10, 页码: UNSP 105316
Authors:  Meng Y(孟宇);  Gu HB(顾洪斌);  Zhuang JH(庄金衡);  Sun WM(孙文明);  Gao ZB(高占彪);  Lian H(连欢);  Yue LJ(岳连捷);  Chang XY(张新宇)
Adobe PDF(3099Kb)  |  Favorite  |  View/Download：377/99  |  Submit date：2019/10/15
Scramjet Combustor Mode Transition Liquid Kerosene Acceleration