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Influence of Doped H2O or H(2)on Soot Production and Power Capability in the Fuel-rich Gas Generator 期刊论文
COMBUSTION SCIENCE AND TECHNOLOGY, 2020, 页码: 12
作者:  Li YJ(李昱君);  Zhang TC(张泰昌);  Yuan T(袁涛);  Fan XJ(范学军)
Adobe PDF(2149Kb)  |  收藏  |  浏览/下载：306/87  |  提交时间：2020/11/30
Soot  fuel-rich combustion  gas generator  power capacity  
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(xfan@imech.ac.cn)
浏览  |  Adobe PDF(1173Kb)  |  收藏  |  浏览/下载：440/216  |  提交时间：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
作者:  Yao W(姚卫);  Fan XJ(范学军)
浏览  |  Adobe PDF(623Kb)  |  收藏  |  浏览/下载：258/87  |  提交时间：2018/01/16
Combustion  Cost Benefit Analysis  Costs  Mixtures  Spacecraft  Supersonic Aircraft  
Development of zone flamelet modelfor scramjet combustor modeling 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);  Fan XJ(范学军)
浏览  |  Adobe PDF(832Kb)  |  收藏  |  浏览/下载：273/81  |  提交时间：2018/11/08
Combustion  Cost benefit analysis  Costs  Mixtures  Ramjet engines  Supersonic aircraft  Computational costs  Equivalence ratios  Local flow conditions  Scramjet combustors  Statistics approaches  Supersonic combustion  Supersonic combustors  Turbulent combustion  
Full-scale Detached Eddy Simulation of kerosene fueled scramjet combustor based on skeletal mechanism 会议论文
20th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, Glasgow, United kingdom, July 6, 2015 - July 9, 2015
作者:  Yao W(姚卫);  Wang J(王晶);  Lu Y(陆阳);  Li XP(李晓鹏);  Fan XJ(范学军)
Adobe PDF(1195Kb)  |  收藏  |  浏览/下载：472/172  |  提交时间：2016/07/01
Adiabatic Flame Temperature  Combustion  Directed Graphs  Flow Separation  Heat Flux  Kerosene  Large Eddy Simulation  Musculoskeletal System  Real Time Systems  Sensitivity Analysis  Spacecraft  Transients  
Development of integrated high temperature sensor for simultaneous measurement of wall heat flux and temperature 期刊论文
REVIEW OF SCIENTIFIC INSTRUMENTS, 2012, 卷号: 83, 期号: 7, 页码: 074901
作者:  Li L(李龙);  Wang J(王晶);  Fan XJ(范学军);  Fan, XJ;  Chinese Acad Sci, Inst Mech, Natl Key Lab High Temp Gas Dynam, 15 Beisihuanxi Rd, Beijing 100190, Peoples R China.
Adobe PDF(2757Kb)  |  收藏  |  浏览/下载：1236/337  |  提交时间：2013/01/18
Radiative Calibration  Facilities  Cavity  Gauge  Meter  Nist