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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
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：323/138  |  Submit date：2016/01/08
Supersonic Combustor  Convective Heat Transfer  Numerical Study  Wall Heat Flux  
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
Authors:  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.
View  |  Adobe PDF(2856Kb)  |  Favorite  |  View/Download：497/149  |  Submit date：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
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：569/235  |  Submit date：2015/06/12
Scramjet  Dual-mode Combustor  Divergent Angle  Cavity Location  Combustion Efficiency  Tdlas