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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
作者:  Wu K(吴坤);  Zhang P(张鹏);  Yao W(姚卫);  Fan XJ(范学军)
浏览  |  Adobe PDF(1820Kb)  |  收藏  |  浏览/下载：454/154  |  提交时间：2018/12/27
Supersonic combustion  Flame stabilization mode  DLR Strut injection scheme  Stagnation Temperature  Overall equivalence ratio  
Prediction of kerosene properties at supercritical pressures by Artificial Neural Network 会议论文
2018 Joint Propulsion Conference, Cincinnati, Ohio. , July 9-11, 2018
作者:  Li B;  Lee YC(李亚超);  Yao W(姚卫);  Lu Y(陆阳);  Fan XJ(范学军)
浏览  |  Adobe PDF(1813Kb)  |  收藏  |  浏览/下载：305/82  |  提交时间：2018/12/26
Prediction of kerosene properties at supercritical pressures by Artificial Neural Network 会议论文
2018 Joint Propulsion Conference, Cincinnati, Ohio., July 9-11, 2018
作者:  Li B(李波);  Lee YC(李亚超);  Yao W(姚卫);  Fan XJ(范学军)
浏览  |  Adobe PDF(1813Kb)  |  收藏  |  浏览/下载：173/64  |  提交时间：2020/08/27
Modeling Analysis of an Actively Cooled Scramjet Combustor Under Different Kerosene/Air Ratios 期刊论文
JOURNAL OF PROPULSION AND POWER, 2018, 卷号: 34, 期号: 4, 页码: 975-991
作者:  Yao W(姚卫);  Lu Y(陆阳);  Wu K(吴坤);  Wang J(王晶);  Fan XJ(范学军)
浏览  |  Adobe PDF(2427Kb)  |  收藏  |  浏览/下载：355/106  |  提交时间：2018/10/19
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
作者:  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)
浏览  |  Adobe PDF(807Kb)  |  收藏  |  浏览/下载：336/104  |  提交时间：2018/07/17
Comparative Study of Elliptic and Round Scramjet Combustors Fueled by RP-3 会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, PEOPLES R CHINA, MAR 06-09, 2017
作者:  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)
浏览  |  Adobe PDF(805Kb)  |  收藏  |  浏览/下载：393/147  |  提交时间：2018/06/06
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：260/89  |  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：274/81  |  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  
Development of a radiative heating system for studies of heat transfer in fuel-cooled structures 会议论文
14th International Energy Conversion Engineering Conference, Salt Lake City, UT, JUL 25-27, 2016
作者:  Dong D(董达);  Lu Y(陆阳);  Yuan YM(袁越明);  Fan XJ(范学军);  Dong, D (reprint author), Chinese Acad Sci, Inst Mech, LHD, Beijing 100190, Peoples R China.
浏览  |  Adobe PDF(637Kb)  |  收藏  |  浏览/下载：290/72  |  提交时间：2017/05/12
Aviation Kerosene  Supercritical Conditions  Pressure  Rp-3  
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：474/173  |  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