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Engine performance analysis and optimization of a dual-mode scramjet with varied inlet conditions 期刊论文
ACTA MECHANICA SINICA, 2016, 卷号: 32, 期号: 1, 页码: 75-82
Authors:  Tian L;  Chen LH(陈立红);  Chen Q(陈强);  Zhong FQ(仲峰泉);  Zhang XY(张新宇);  Chen, LH (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
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Dual-mode Scramjet  Engine Performance  Thrust  Optimization  Heat Release Distribution  Simulated Annealing Algorithm  
Quasi-One-Dimensional Multimodes Analysis for Dual-Mode Scramjet 期刊论文
JOURNAL OF PROPULSION AND POWER, 2014, 卷号: 30, 期号: 6, 页码: 1559-1567
Authors:  Tian L;  Chen LH(陈立红);  Chen Q(陈强);  Li F(李飞);  Zhang XY(张新宇);  Tian, L (reprint author), Chinese Acad Sci, State Key Lab High Temp Gas Dynam, Inst Mech, Beijing 100190, Peoples R China.
Adobe PDF(7587Kb)  |  Favorite  |  View/Download：598/137  |  Submit date：2014/12/18
Laser Diagnostics of Combustion Enhancement on a CH4/Air Bunsen Flame by Dielectric Barrier Discharge 期刊论文
CHINESE PHYSICS LETTERS, 2013, 卷号: 30, 期号: 8, 页码: 085203/1-085203/4
Authors:  Zhang SH(张少华);  Yu XL(余西龙);  Chen LH(陈立红);  Zhang XY(张新宇);  Yu, XL (reprint author), Chinese Acad Sci, Inst Mech, Beijing 100190, Peoples R China.
Adobe PDF(1970Kb)  |  Favorite  |  View/Download：858/272  |  Submit date：2013/09/27
Premixed Flames  Plasma  Methane  Mixtures  Planar Laser Induced Fluorescence  Laser Diagnostics  Flame Velocities  Emission Spectra  Dielectric Barrier Discharge  
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
Authors:  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.
View  |  Adobe PDF(1235Kb)  |  Favorite  |  View/Download：1340/425  |  Submit date：2013/07/30
Scramjet  Kerosene Fuel  Plasma Torch  Ignition  
Numerical simulation of ignition and combustion of ethylene in a supersonic model combustor with a reduced kinetic mechanism 期刊论文
COMBUSTION SCIENCE AND TECHNOLOGY, 2013, 卷号: 185, 期号: 4, 页码: 548-563
Authors:  Zhong FQ(仲峰泉);  Chen LH(陈立红);  Li F(李飞);  Zhang XY(张新宇);  Sung CJ;  Zhong, FQ (reprint author), Chinese Acad Sci, State Key Lab High Temp Gas Dynam, Inst Mech, Beijing 100190, Peoples R China.
Adobe PDF(1454Kb)  |  Favorite  |  View/Download：1437/490  |  Submit date：2013/05/03
Ethylene  Ignition  Numerical Simulation  Reduced Kinetic Mechanism  Supersonic Combustion  
考虑煤油裂解效应的超声速燃烧室再生冷却过程分析 期刊论文
推进技术, 2013, 卷号: 34, 期号: 1, 页码: 47-53
Authors:  王曦;  仲峰泉;  陈立红;  张新宇
Adobe PDF(779Kb)  |  Favorite  |  View/Download：1196/386  |  Submit date：2013/03/07
超声速燃烧室  耦合传热  再生冷却  超临界态  催化裂解  
Study on Judgment Method of Combustion Mode on Dual-mode Scramjet 期刊论文
Procedia Engineering, 2013, 卷号: 67, 页码: 147-154
Authors:  Chen Q(陈强);  Chen LH(陈立红);  Gu HB(顾洪斌);  Zhang XY(张新宇);  Wang P
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Scramjet  Artificial Neural Network  
Simultaneous measurements of multiple flow parameters for scramjet characterization using tunable diode-laser sensors 期刊论文
Applied Optics, 2011, 卷号: 50, 期号: 36, 页码: 6697-6707
Authors:  Li F(李飞);  Yu XL(余西龙);  Gu HB(顾洪斌);  Li Z(李智);  Zhao Y;  Ma L;  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
Adobe PDF(1090Kb)  |  Favorite  |  View/Download：1211/258  |  Submit date：2012/04/01
Absorption-spectroscopy  Water-vapor  Temperature Distributions  Gas Temperature  Combustion  Cavity  Operation  Engines  Model  
释热分布对超燃冲压发动机性能的影响及优化 期刊论文
推进技术, 2009, 卷号: 30, 期号: 2, 页码: 135-138
Authors:  陈强;  陈立红;  顾洪斌;  张新宇
Adobe PDF(415Kb)  |  Favorite  |  View/Download：669/207  |  Submit date：2010/05/03
超燃冲压发动机  推力性能  释热分布  模拟退火算法  
Experimental investigation on the cavity-based scramjet model 期刊论文
CHINESE SCIENCE BULLETIN, 2009, 卷号: 54, 期号: 16, 页码: 2794-2799
Authors:  Gu HB(顾洪斌);  Chen LH(陈立红);  Zhang XY(张新宇);  Gu HB(顾洪斌)
View  |  Adobe PDF(627Kb)  |  Favorite  |  View/Download：1181/326  |  Submit date：2009/09/28
Scramjet  Combustor  Cavity  Performance