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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
作者:  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  
一种液氧气化器装置 专利
专利类型: 一种液氧气化器装置, 专利号: ZL201410347497.4, 公开日期: 2014-07-21
发明人:  陆阳;  姚卫;  孟令瑾;  袁涛;  范学军
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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
作者:  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  
一种用于超声速燃烧直联的异丁烷供给系统 专利
专利类型: 一种用于超声速燃烧直联的异丁烷供给系统, 专利号: ZL201410586753.5, 公开日期: 2014-10-28
发明人:  袁涛;  李龙;  范学军;  孟令瑾;  谢巍;  朱文忠
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高度欠膨胀声速射流的自相似特性 期刊论文
航空动力学报, 2017, 卷号: 32, 期号: 01, 页码: 177-187
作者:  李晓鹏;  姚卫;  范学军
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高度欠膨胀射流  大涡模拟  自相似特性  高斯拟合  剪切层发展  
一种流场和火焰结构同步探测方法 专利
专利类型: 一种流场和火焰结构同步探测方法, 专利号: ZL201410373701.X, 公开日期: 2014-07-31
发明人:  袁越明;  张泰昌;  宋军浩;  范学军
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Development and Fidelity Evaluation of a Skeletal Ethylene Mechanism under Scramjet-Relevant Conditions 期刊论文
ENERGY & FUELS, 2017, 卷号: 31, 期号: 12, 页码: 14296
作者:  Wu K(吴坤);  Yao W(姚卫);  Fan XJ(范学军);  Yao, W;  Fan, XJ
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Numerical Investigation on Flame Stabilization in DLR Hydrogen Supersonic Combustor with Strut Injection 期刊论文
COMBUSTION SCIENCE AND TECHNOLOGY, 2017, 卷号: 189, 期号: 12, 页码: 2154-2179
作者:  Wu, Kun;  Zhang, Peng;  Yao W(姚卫);  Fan XJ(范学军);  Zhang, P (reprint author), Hong Kong Polytech Univ, Dept Mech Engn, Hong Kong 999077, Hong Kong, Peoples R China.
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Detailed Hydrogen Oxidation Mechanism  Dlr  Flame Stabilization  Sensitivity Analysis  Supersonic Combustion  
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
作者:  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.
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Supersonic Combustion  Flame Stabilization  Stagtnation Temperature  Gloabal Equivalence Ratio  Ch** Ch*emiluminesenCh*e  
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
作者:  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(
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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