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Method of Selecting Active Parameters Using Sensitivity Analysis and Linear Programming 期刊论文
COMBUSTION SCIENCE AND TECHNOLOGY, 2023, 页码: 17
Authors:  Li YJ(李昱君);  Zhang TC(张泰昌);  Fang, Yunming;  Fan XJ(范学军)
Adobe PDF(3807Kb)  |  Favorite  |  View/Download：98/9  |  Submit date：2023/11/28
Active parameter  sensitivity analysis  linear programming  selection method  chemical kinetic model  
Atomization of misaligned impinging liquid jets 期刊论文
PHYSICS OF FLUIDS, 2021, 卷号: 33, 期号: 9, 页码: 15
Authors:  Zhang, Chenwei;  Zhang ZY(张振宇);  Wu K(吴坤);  Xia, Xi;  Fan XJ(范学军)
Adobe PDF(15401Kb)  |  Favorite  |  View/Download：268/66  |  Submit date：2022/01/12
AMP Exception  AMP Exception  
A one-dimensional transient calculation method for flow instability of supercritical hydrocarbon in cooling channels 会议论文
AIAA Propulsion and Energy Forum, VIRTUAL EVENT, 2021年8月9-11日
Authors:  Jin YC(靳一超);  Wu K(吴坤);  Lu Y(陆阳);  Fan XJ(范学军)
Adobe PDF(1121Kb)  |  Favorite  |  View/Download：180/49  |  Submit date：2022/07/04
Flow Modulation and Mixing Enhancement of Highly Underexpanded Jet by Vortex Excitation 期刊论文
AIAA JOURNAL, 2020, 卷号: 58, 期号: 6, 页码: 2462-2474
Authors:  Wang Y(汪也);  Wu K(吴坤);  Yao W(姚卫);  Fan XJ(范学军)
Adobe PDF(6305Kb)  |  Favorite  |  View/Download：368/95  |  Submit date：2020/07/06
Hypergolic ignition modulated by head-on collision, intermixing and convective cooling of binary droplets with varying sizes 期刊论文
INTERNATIONAL JOURNAL OF HEAT AND MASS TRANSFER, 2019, 卷号: 139, 页码: 475-481
Authors:  Zhang DW;  Yu DH;  Zhang P;  Yuan YM(袁越明);  Yue LJ(岳连捷);  Zhang TC(张泰昌);  Fan XJ(范学军)
Adobe PDF(1528Kb)  |  Favorite  |  View/Download：343/127  |  Submit date：2019/09/09
Computational realization of multiple flame stabilization modes in DLR strut-injection hydrogen supersonic combustor 期刊论文
PROCEEDINGS OF THE COMBUSTION INSTITUTE, 2019, 卷号: 37, 期号: 3, 页码: 3685-3692
Authors:  Wu K(吴坤);  Zhang P(张鹏);  Yao W(姚卫);  Fan XJ(范学军)
Adobe PDF(1820Kb)  |  Favorite  |  View/Download：483/162  |  Submit date：2018/12/27
Supersonic combustion  Flame stabilization mode  DLR Strut injection scheme  Stagnation Temperature  Overall equivalence ratio  
Comparative Study of Elliptic and Round Scramjet Combustors Fueled by RP-3 期刊论文
JOURNAL OF PROPULSION AND POWER, 2018, 卷号: 34, 期号: 3, 页码: 772-786
Authors:  Yao W(姚卫);  Yuan YM(袁越明);  Li XP(李晓鹏);  Wang J(王晶);  Wu K(吴坤);  Fan XJ(范学军)
Adobe PDF(807Kb)  |  Favorite  |  View/Download：368/118  |  Submit date：2018/07/17
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)
Adobe PDF(1173Kb)  |  Favorite  |  View/Download：476/230  |  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  
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)
Adobe PDF(1249Kb)  |  Favorite  |  View/Download：331/100  |  Submit date：2018/01/16
Combustion  Diesel Engines  Hydrogen  Large Eddy Simulation  Spacecraft  Stabilization  Supersonic Aircraft  Temperature Measurement  Wall Flow  
Characterization of flame stabilization modes in an ethylene-fueled supersonic combustor using time-resolved CH* chemiluminescence 期刊论文
PROCEEDINGS OF THE COMBUSTION INSTITUTE, 2017, 卷号: 36, 期号: 2, 页码: 2919-2925
Authors:  Yuan YM(袁越明);  Zhang TC(张泰昌);  Yao W(姚卫);  Fan XJ(范学军);  Zhang P(张鹏);  Fan, XJ (reprint author), Chinese Acad Sci, State Key Lab High Temp Gas Dynam, Beijing 100190, PR, Peoples R China.
Adobe PDF(1681Kb)  |  Favorite  |  View/Download：331/104  |  Submit date：2017/12/27
Supersonic Combustion  Flame Stabilization  Stagtnation Temperature  Gloabal Equivalence Ratio  Ch** Ch*emiluminesenCh*e