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Combustion performance of a novel hybrid rocket fuel grain with a nested helical structure 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2020, 卷号: 97, 页码: 8
作者:  Wang ZZ(王泽众);  Lin X(林鑫);  Li F(李飞);  Yu XL(余西龙)
Adobe PDF(1961Kb)  |  收藏  |  浏览/下载：262/101  |  提交时间：2020/05/18
Hybrid rocket engine  Paraffin-based fuel  Acrylonitrile-butadiene-styrene  Regression rate  Combustion efficiency  
Effect of the fuel-air flow velocity on heat release rate of swirling non-premixed methane flames 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2019, 卷号: 95, 页码: UNSP 105465
作者:  Wang KL(王宽亮);  Li F(李飞);  Zou PF(邹鹏飞);  Lin X(林鑫);  Mao RH(毛荣海);  Yu XL(余西龙)
浏览  |  Adobe PDF(2678Kb)  |  收藏  |  浏览/下载：251/61  |  提交时间：2020/03/21
Swirl flame  Heat release  Chemiluminescence  3D-CTC  
Effect of the fuel-air flow velocity on heat release rate of swirling non-premixed methane flames 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2019, 卷号: 95, 页码: UNSP 105465
作者:  Wang KL(王宽亮);  Li F(李飞);  Zou PF(邹鹏飞);  Lin X(林鑫);  Mao RH(毛荣海);  Yu XL(余西龙)
浏览  |  Adobe PDF(2678Kb)  |  收藏  |  浏览/下载：200/67  |  提交时间：2020/03/21
Swirl flame  Heat release  Chemiluminescence  3D-CTC  
Tunable diode laser absorption spectroscopy measurements of high-pressure ammonium dinitramide combustion 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2015, 卷号: 45, 页码: 140-149
作者:  Yao, Zhaopu;  Zhang, Wei;  Wang, Meng;  Chen, Jun;  Shen, Yan;  Wei, Yanming;  Yu XL(余西龙);  Li F(李飞);  Ceng H(曾徽);  Yu, XL (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
Unknown(1847Kb)  |  收藏  |  浏览/下载：238/69  |  提交时间：2015/10/21
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：534/225  |  提交时间：2015/06/12
Scramjet  Dual-mode Combustor  Divergent Angle  Cavity Location  Combustion Efficiency  Tdlas  
Plasma-assisted ignition for a kerosene fueled scramjet at Mach 1.8 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2013, 卷号: 28, 期号: 1, 页码: 72-78
作者:  Li F(李飞);  Yu XL(余西龙);  Tong YG(仝颖刚);  Shen Y(沈岩);  Chen J(陈健);  Chen LH(陈立红);  Zhang XY(张新宇);  Yu, XL (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
浏览  |  Adobe PDF(1235Kb)  |  收藏  |  浏览/下载：1278/408  |  提交时间：2013/07/30
Scramjet  Kerosene Fuel  Plasma Torch  Ignition