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Numerical study of inflow equivalence ratio inhomogeneity on oblique detonation formation in hydrogen-air mixtures 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2017, 卷号: 71, 页码: 256-263
Authors:  Fang YS(方宜申);  Hu ZM(胡宗民);  Teng HH(滕宏辉);  Jiang ZL(姜宗林);  Ng HD
View  |  Adobe PDF(2663Kb)  |  Favorite  |  View/Download：405/103  |  Submit date：2018/02/08
Oblique Detonation  Equivalence Ratio  Mixture Inhomogeneity  Detailed Chemistry  
The dual information preserving method for stiff reacting flows 期刊论文
COMPUTERS & FLUIDS, 2017, 卷号: 157, 页码: 253-275
Authors:  Liu, Li;  Shen YQ(申义庆);  Liu, Shengping;  Yu, Ming;  Shen, YQ (reprint author), Chinese Acad Sci, Inst Mech, LHD, Beijing 100190, Peoples R China.
View  |  Adobe PDF(5104Kb)  |  Favorite  |  View/Download：448/150  |  Submit date：2017/11/16
Stiff Reacting Flow  Dual Information Preserving Method  Numerical Perturbation Method  Shock-capturing Scheme  
The design and main performance of a hydrogen peroxide/kerosene coaxial-swirl injector in a lab-scale rocket engine 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2017, 卷号: 70, 页码: 636-643
Authors:  Li HX(李慧鑫);  Ye L(叶亮);  Wei XL(魏小林);  Li T(李腾);  Li S(李森);  Wei, XL (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, 15 Beisihuanxi Rd, Beijing 100190, Peoples R China.
View  |  Adobe PDF(1708Kb)  |  Favorite  |  View/Download：502/217  |  Submit date：2017/12/18
H2o2/kerosene Bipropellant  Coaxial-swirl Injector  Geometric Constant  Performance  
Flow characteristic of highly underexpanded jets from various nozzle geometries 期刊论文
APPLIED THERMAL ENGINEERING, 2017, 卷号: 125, 页码: 240-253
Authors:  Li XP(李晓鹏);  Zhou, Rui;  Yao W(姚卫);  Fan XJ(范学军);  Fan, XJ (reprint author), Chinese Acad Sci, State Key Lab High Temp Gas Dynam, Inst Mech, Beijing 100190, Peoples R China.
View  |  Adobe PDF(5723Kb)  |  Favorite  |  View/Download：455/196  |  Submit date：2017/11/16
Underexpanded Jets  Noncircular Jets  Nozzle Geometry  Large Eddy Simulation  
Three-dimensional flame measurements with large field angle 期刊论文
OPTICS EXPRESS, 2017, 卷号: 25, 期号: 18, 页码: 21008-21018
Authors:  Wang KL(王宽亮);  Li F(李飞);  Ceng H(曾徽);  Yu XL(余西龙);  Li, F (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
View  |  Adobe PDF(2976Kb)  |  Favorite  |  View/Download：362/116  |  Submit date：2017/11/16
Initiation structure of oblique detonation waves behind conical shocks 期刊论文
PHYSICS OF FLUIDS, 2017, 卷号: 29, 期号: 8
Authors:  Yang PF(杨鹏飞);  Ng, Hoi Dick;  Teng HH(滕宏辉);  Jiang ZL(姜宗林);  Teng, HH (reprint author), Beijing Inst Technol, Sch Aerosp Engn, Dept Mech, Beijing 100081, Peoples R China.
View  |  Adobe PDF(5788Kb)  |  Favorite  |  View/Download：481/109  |  Submit date：2017/11/16
A comparative study of elliptical and round scramjet combustors by Improved Delayed Detached Eddy Simulation 会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017
Authors:  Yao W(姚卫);  Yuan YM(袁越明);  Li XP(李晓鹏);  Wang J(王晶);  Fan XJ(范学军);  Fan, Xuejun(xfan@imech.ac.cn)
View  |  Adobe PDF(1173Kb)  |  Favorite  |  View/Download：485/234  |  Submit date：2018/01/16
Adiabatic Flame Temperature  Aerodynamics  Boundary Layer Flow  Boundary Layers  Chemical Analysis  Combustion  Computational Chemistry  Directed Graphs  Flow Separation  Mach Number  Principal Component Analysis  Regression Analysis  Sensitivity Analysis  Spacecraft  Supersonic Aerodynamics  Supersonic Aircraft  Transients  
Development of zone flamelet model for scramjet combustor modeling 会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017
Authors:  Yao W(姚卫);  Fan XJ(范学军)
View  |  Adobe PDF(623Kb)  |  Favorite  |  View/Download：298/105  |  Submit date：2018/01/16
Combustion  Cost Benefit Analysis  Costs  Mixtures  Spacecraft  Supersonic Aircraft  
LES Study of Flame Stabilization in DLR Hydrogen Supersonic Combustor with Strut Injection 会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017
Authors:  Wu K(吴坤);  Zhang P(张鹏);  Yao W(姚卫);  Fan XJ(范学军);  Zhang, Peng(pengzhang.zhang@polyu.edu.hk)
View  |  Adobe PDF(1249Kb)  |  Favorite  |  View/Download：340/105  |  Submit date：2018/01/16
Combustion  Diesel Engines  Hydrogen  Large Eddy Simulation  Spacecraft  Stabilization  Supersonic Aircraft  Temperature Measurement  Wall Flow  
圆球诱发斜爆轰波的数值研究 期刊论文
力学学报, 2017, 卷号: 49, 期号: 02, 页码: 268-273
Authors:  方宜申;  胡宗民;  滕宏辉;  姜宗林
View  |  Adobe PDF(489Kb)  |  Favorite  |  View/Download：366/84  |  Submit date：2017/12/22
斜爆轰  氢氧  起爆  熄爆