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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.
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Underexpanded Jets  Noncircular Jets  Nozzle Geometry  Large Eddy Simulation  
Numerical investigation of characteristic frequency excited highly underexpanded jets 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2017, 卷号: 63, 页码: 304-316
Authors:  Li XP;  Fan E;  Yao W(姚卫);  Fan XJ(范学军);  Fan, XJ (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.;  Fan, XJ (reprint author), Univ Chinese Acad Sci, Sch Engn Sci, Beijing 100049, Peoples R China.
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Fuel Jets  Underexpanded Jets  Jet Mixing Control  Excited Jets  Large Eddy Simulation  
A comparative study of highly underexpanded nitrogen and hydrogen jets using large eddy simulation 期刊论文
INTERNATIONAL JOURNAL OF HYDROGEN ENERGY, 2016, 卷号: 41, 期号: 9, 页码: 5151-5161
Authors:  Li XP(李晓鹏);  Wu K(吴坤);  Yao W(姚卫);  Fan XJ(范学军);  Li, XP (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
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Scramjet  Hydrogen  Highly Underexpanded Jet  Large Eddy Simulation  
Large-Eddy Simulation of Time Evolution and Instability of Highly Underexpanded Sonic Jets 期刊论文
AIAA JOURNAL, 2016, 卷号: 54, 期号: 10, 页码: 3191-3211
Authors:  Li XP(李晓鹏);  Yao W(姚卫);  Fan XJ(范学军);  Li, XP (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
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Blowout Limits of Cavity-Stabilized Flame of Supercritical Kerosene in Supersonic Combustors 期刊论文
Journal of Propulsion and Power, 2014, 卷号: 30, 期号: 5, 页码: 1161-1166
Authors:  Zhang TC(张泰昌);  Wang J(王晶);  Qi L;  Fan XJ(范学军);  Zhang P;  Fan, XJ (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, 15 Beisihuanxi Rd, Beijing 100190, Peoples R China.
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Thermal Cracking and Heat Sink Capacity of Aviation Kerosene Under Supercritical Conditions 会议论文
AIAA/ASME/SAE/ASEE 45th Joint Propulsion Conference and Exhibit, Denver, CO, AUG 02-08, 2009
Authors:  Zhong FQ(仲峰泉);  Fan XJ(范学军);  Yu G(俞刚);  Li JG(李建国);  Sung CJ;  Zhong, FQ (reprint author), Chinese Acad Sci, Inst Mech, Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China
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Thermal Cracking and Heat Sink Capacity of Aviation Kerosene Under Supercritical Conditions 期刊论文
Journal of Thermophysics and Heat Transfer, 2011, 卷号: 25, 期号: 3, 页码: 450-456
Authors:  Zhong FQ(仲峰泉);  Fan XJ(范学军);  Yu G(俞刚);  Li JG(李建国);  Sung CJ;  Zhong, FQ (reprint author), Chinese Acad Sci, Inst Mech, Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China
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Tetralin  Decalin  
Convective heat transfer characteristics of China RP-3 aviation kerosene at supercritical pressure 期刊论文
Applied Thermal Engineering, 2011, 卷号: 31, 期号: 14-15, 页码: 2360-2366
Authors:  Li XF;  Huai XL;  Cai J;  Zhong FQ(仲峰泉);  Fan XJ(范学军);  Guo ZX;  Huai, XL (reprint author), Chinese Acad Sci, Inst Engn Thermophys, Beijing 100190, Peoples R China
Adobe PDF(289Kb)  |  Favorite  |  View/Download:1304/414  |  Submit date:2012/04/01
Supercritical Pressure  Aviation Kerosene  Convective Heat Transfer  Numerical Study  Cracked Kerosene  Tubes  Water  Flows  
CFD Simulation of Kerosene-Fueled Supersonic Combustion Ramjet Combustor Experiments 会议论文
Asia-Pacific International Symposium on Aerospace Technology, Xian, PEOPLES R CHINA, SEP 13-15, 2010
Authors:  Wan T(万田);  Chen LH(陈立红);  Wang J(王晶);  Fan XJ(范学军);  Zhang XY(张新宇);  Wan, TA (reprint author), Chinese Acad Sci, Inst Mech, Key Lab High Temp Gas Dynam LHD, Beijing 100190, Peoples R China.
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Effects of entry conditions on cracked kerosene-fueled supersonic combustor performance 期刊论文
Combustion Science and Technology, 2007, 卷号: 179, 期号: 10, 页码: 2199-2217
Authors:  Fan XJ(范学军);  Yu G(俞刚);  Li JG(李建国);  Yue LJ(岳连捷);  Zhang XY(张新宇);  Sung CJ;  Fan, XJ (reprint author), Chinese Acad Sci, Inst Mech, Beijing 100080, Peoples R China.
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Entry Conditions  Kerosene  Supersonic Combustion  Thermal Cracking  Model Combustor  Propulsion  Injection