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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.
浏览  |  Adobe PDF(5723Kb)  |  收藏  |  浏览/下载:102/38  |  提交时间:2017/11/16
Underexpanded Jets  Noncircular Jets  Nozzle Geometry  Large Eddy Simulation  
一种液氧气化器装置 专利
专利类型: 发明专利. 一种液氧气化器装置, 专利号: ZL201410347497.4, 申请日期: 2014-07-21, 授权日期: 2017-06-30
发明人:  陆阳;  姚卫;  孟令瑾;  袁涛;  范学军
浏览  |  Adobe PDF(448Kb)  |  收藏  |  浏览/下载:121/24  |  提交时间:2017/07/18
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.
浏览  |  Adobe PDF(3588Kb)  |  收藏  |  浏览/下载:87/25  |  提交时间:2017/07/24
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: 发明专利. 一种用于超声速燃烧直联的异丁烷供给系统, 专利号: ZL201410586753.5, 申请日期: 2014-10-28, 授权日期: 2017-02-08
发明人:  袁涛;  李龙;  范学军;  孟令瑾;  谢巍;  朱文忠
浏览  |  Adobe PDF(841Kb)  |  收藏  |  浏览/下载:119/25  |  提交时间:2017/02/21
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
浏览  |  Adobe PDF(767Kb)  |  收藏  |  浏览/下载:56/13  |  提交时间:2017/12/22
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: 发明专利. 一种流场和火焰结构同步探测方法, 专利号: ZL201410373701.X, 申请日期: 2014-07-31, 授权日期: 2017-01-18
发明人:  袁越明;  张泰昌;  宋军浩;  范学军
浏览  |  Adobe PDF(694Kb)  |  收藏  |  浏览/下载:111/20  |  提交时间:2017/02/21
A low-dissipation scheme based on OpenFoam designed for large eddy simulation in compressible flow 会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017
作者:  Lee YC;  Yao W(姚卫);  Fan XJ(范学军);  Yao, Wei(weiyao@imech.ac.cn)
浏览  |  Adobe PDF(1358Kb)  |  收藏  |  浏览/下载:73/12  |  提交时间:2018/01/16
Computational Fluid Dynamics  Computer Software  Digital Storage  Kinetic Energy  Kinetics  Open Source Software  Open Systems  Runge Kutta Methods  Shock Tubes  Shock Waves  Spacecraft  Turbulence  Two Phase Flow  
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
作者:  Yao W(姚卫);  Fan XJ(范学军)
浏览  |  Adobe PDF(623Kb)  |  收藏  |  浏览/下载:43/15  |  提交时间:2018/01/16
Combustion  Cost Benefit Analysis  Costs  Mixtures  Spacecraft  Supersonic Aircraft  
Experimental Studies of Film Cooling in Supersonic Combustors 会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017
作者:  Fan C(樊川);  Wang J(王晶);  Fan XJ(范学军)
浏览  |  Adobe PDF(735Kb)  |  收藏  |  浏览/下载:60/22  |  提交时间:2018/01/16
Combustion  Combustors  Coolants  Kerosene  Spacecraft  Supersonic Aerodynamics  
A comparative study of elliptic and round scramjet combustors by improved delayed detached Eddy simulation 会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Hypersonics 2017, Xiamen, China, March 6, 2017 - March 9, 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)
浏览  |  Adobe PDF(1193Kb)  |  收藏  |  浏览/下载:12/1  |  提交时间:2018/11/08
Adiabatic flame temperature  Boundary layer flow  Boundary layers  Chemical analysis  Computational chemistry  Directed graphs  Flow separation  Mach number  Principal component analysis  Regression analysis  Sensitivity analysis  Supersonic aerodynamics  Supersonic aircraft  Boundary layer thickness  Combustion characteristics  Combustion performance  Directed relation graph  Heat Release Rate (HRR)  Improved delayed detached eddy simulations  Proper orthogonal decomposition method  Supersonic combustors