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Numerical study of combustion and convective heat transfer of a Mach 2.5 supersonic combustor 期刊论文
APPLIED THERMAL ENGINEERING, 2015, 卷号: 89, 页码: 883-896
作者:  Wang X;  Zhong FQ(仲峰泉);  Gu HB(顾宏斌);  Zhang XY(张新宇);  Zhong, FQ (reprint author), 15 Beisihuanxi Rd, Beijing 100190, Peoples R China.
浏览  |  Adobe PDF(4711Kb)  |  收藏  |  浏览/下载：296/129  |  提交时间：2016/01/08
Supersonic Combustor  Convective Heat Transfer  Numerical Study  Wall Heat Flux  
Development of efficient and accurate skeletal mechanisms for hydrocarbon fuels and kerosene surrogate 期刊论文
ACTA MECHANICA SINICA, 2015, 卷号: 31, 期号: 5, 页码: 732-740
作者:  Zhong FQ(仲峰泉);  Ma SG;  Zhang XY(张新宇);  Sung CJ;  Niemeyer KE;  Zhong, FQ (reprint author), Chinese Acad Sci, State Key Lab High Temp Gas Dynam, Inst Mech, Beijing 100190, Peoples R China.
浏览  |  Adobe PDF(1318Kb)  |  收藏  |  浏览/下载：285/90  |  提交时间：2016/01/08
Reduced Chemistry  Hydrocarbons  Directed Relation Graph  Ignition Delay Time  
Numerical study of heat transfer deterioration of turbulent supercritical kerosene flow in heated circular tube 期刊论文
INTERNATIONAL JOURNAL OF HEAT AND MASS TRANSFER, 2015, 卷号: 85, 页码: 1003-1011
作者:  Dang GX;  Zhong FQ(仲峰泉);  Zhang YJ;  Zhang XY(张新宇);  Zhong, FQ (reprint author), Chinese Acad Sci, Inst Mech, Bei Si Huan Xi Rd 15, Beijing 100190, Peoples R China.
浏览  |  Adobe PDF(2856Kb)  |  收藏  |  浏览/下载：458/133  |  提交时间：2015/06/12
Supercritical Kerosene  Convective Heat Transfer  Turbulent Flow  Numerical Study  
Experimental study on the effect of combustor configuration on the performance of dual-mode combustor 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2015, 卷号: 42, 页码: 169-175
作者:  Wang ZP(王知溥);  Li F(李飞);  Gu HS;  Yu XL(余西龙);  Zhang XY(张新宇);  Li, F (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
浏览  |  Adobe PDF(1112Kb)  |  收藏  |  浏览/下载：536/225  |  提交时间：2015/06/12
Scramjet  Dual-mode Combustor  Divergent Angle  Cavity Location  Combustion Efficiency  Tdlas  
Numerical analysis on the heat transfer of three types of nozzles for the hypersonic long-run wind tunnel 期刊论文
Science China-Technological Sciences, 2015, 卷号: 58, 期号: 3, 页码: 470-475
作者:  Xing YF(邢云绯);  Zhong FQ(仲峰泉);  Li DX(李东霞);  Zhang XY(张新宇);  Zhong, FQ (reprint author), Chinese Acad Sci, Inst Mech, Natl Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
浏览  |  Adobe PDF(860Kb)  |  收藏  |  浏览/下载：438/187  |  提交时间：2015/04/28
Hypersonic Scramjet Test Tunnel  Nozzle  Aerodynamic Heating  Convective Heat Transfer  
Large eddy simulation of ignition and combustion of ethylene/air turbulent jet diffusion flame with reduced kinetic mechanism 会议论文
20th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, 2015, Glasgow, United kingdom, July 6, 2015 - July 9, 2015
作者:  Ma SG(马素刚);  Zhong FQ(仲峰泉);  Zhang XY(张新宇);  Zhong, Fengquan (fzhong@imech.ac.cn)
浏览  |  Adobe PDF(496Kb)  |  收藏  |  浏览/下载：244/72  |  提交时间：2017/05/05
Combustion Pro  Cess  Directed Relation Graph  Dynamic Evolution  Fuel Injection Velocities  Kinetic Mechanism  Reduced Mechanisms  Temperature Profiles  Temporal And Spatial Evolutions