IMECH-IR

Browse/Search Results:  1-5 of 5 Help

Filters            
Selected(0)Clear Items/Page:    Sort:
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
Authors:  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.
View  |  Adobe PDF(4711Kb)  |  Favorite  |  View/Download:319/137  |  Submit date: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
Authors:  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.
View  |  Adobe PDF(1318Kb)  |  Favorite  |  View/Download:312/102  |  Submit date:2016/01/08
Reduced Chemistry  Hydrocarbons  Directed Relation Graph  Ignition Delay Time  
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
Authors:  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.
View  |  Adobe PDF(1112Kb)  |  Favorite  |  View/Download:564/233  |  Submit date:2015/06/12
Scramjet  Dual-mode Combustor  Divergent Angle  Cavity Location  Combustion Efficiency  Tdlas  
Experimental study of combustion oscillations in a dual-mode scramjet 会议论文
20th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, 2015, 2015
Authors:  Tian XD;  Chen LH(陈立红);  Gu HB(顾洪斌);  Liu C;  Cheng LW;  Chang XY(张新宇);  Chen, Lihong (lhchen@imech.ac.cn)
View  |  Adobe PDF(824Kb)  |  Favorite  |  View/Download:252/73  |  Submit date:2017/09/04
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
Authors:  Ma SG(马素刚);  Zhong FQ(仲峰泉);  Zhang XY(张新宇);  Zhong, Fengquan (fzhong@imech.ac.cn)
View  |  Adobe PDF(496Kb)  |  Favorite  |  View/Download:267/77  |  Submit date:2017/05/05
Combustion Pro  Cess  Directed Relation Graph  Dynamic Evolution  Fuel Injection Velocities  Kinetic Mechanism  Reduced Mechanisms  Temperature Profiles  Temporal And Spatial Evolutions