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Coupling Effect of Multicavity on Flame Stabilization Mode Transitions in Scramjet Combustor 期刊论文
JOURNAL OF PROPULSION AND POWER, 2023./通讯作者：Zhang, QF
Authors:  Wu ZJ(吴振杰);  Zhang QF(张启帆);  Yu FY(于方游);  Luo WH(罗苇航);  Gao ZB(高占彪);  Yue LJ(岳连捷)
Adobe PDF(582Kb)  |  Favorite  |  View/Download：67/12  |  Submit date：2023/06/15
Scramjet Engines  Combustor Design  flame stabilization mode  transition  path dependence  
Effect of combustion mode on thrust performance in a symmetrical tandem-cavity scramjet combustor 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2022, 卷号: 130, 页码: 11./通讯作者：Sun, Mingbo, Zhao, Guoyan
Authors:  Liu, Mingjiang;  Sun, Mingbo;  Zhao, Guoyan;  Meng Y(孟宇);  Huang, Yuhui;  Ma, Guangwei;  Wang, Hongbo
Adobe PDF(3841Kb)  |  Favorite  |  View/Download：192/42  |  Submit date：2022/12/20
Tandem-cavity  Scramjet combustor  Combustion mode  Thrust performance  
Investigation for Effects of Jet Scale on Flame Stabilization in Scramjet Combustor 期刊论文
ENERGIES, 2022, 卷号: 15, 期号: 10, 页码: 16./通讯作者：Gu, Hongbin
Authors:  Li Z(李桢);  Gu HB(顾洪斌)
Adobe PDF(7637Kb)  |  Favorite  |  View/Download：338/127  |  Submit date：2022/07/18
scramjet combustor  direct-connect test  jet scale  flame stabilization  
Improved delayed detached eddy simulation of supersonic combustion fueled by liquid kerosene 期刊论文
FUEL, 2022, 卷号: 313, 页码: 13./通讯作者：Huang, Yue, Yao, Wei
Authors:  Shen, Wubingyi;  Huang, Yue;  Yao W(姚卫);  Liu, Hedong;  You, Yancheng
Adobe PDF(9915Kb)  |  Favorite  |  View/Download：263/62  |  Submit date：2022/05/17
Improved delayed detached eddy simulation  Liquid kerosene  Skeletal reaction mechanism  Equivalence ratio  Cavity-based scramjet combustor  Supersonic combustion  
Experimental study of mode transition characteristics of a cavity-based scramjet combustor during acceleration 期刊论文
Aerospace Science and Technology, 2019, 卷号: 93, 期号: 10, 页码: UNSP 105316./通讯作者：顾洪斌
Authors:  Meng Y(孟宇);  Gu HB(顾洪斌);  Zhuang JH(庄金衡);  Sun WM(孙文明);  Gao ZB(高占彪);  Lian H(连欢);  Yue LJ(岳连捷);  Chang XY(张新宇)
View  |  Adobe PDF(3099Kb)  |  Favorite  |  View/Download：397/105  |  Submit date：2019/10/15
Scramjet Combustor Mode Transition Liquid Kerosene Acceleration  
Development of Skeletal Kerosene Mechanisms and Application to Supersonic Combustion 期刊论文
ENERGY & FUELS, 2018, 页码: 10.1021/acs.energyfuels.8b03350
Authors:  Yao W(姚卫);  Wu K(吴坤);  Fan XJ(范学军)
View  |  Adobe PDF(1388Kb)  |  Favorite  |  View/Download：383/126  |  Submit date：2018/12/27
Combustion Condition  Combustor Efficiency  Improved Delayed Detached Eddy Simulations  Initial Temperatures  Laminar Flame Speed  Scramjet Combustors  Supersonic Combustion  Turbulence-chemistry Interactions  
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：627/243  |  Submit date：2015/06/12
Scramjet  Dual-mode Combustor  Divergent Angle  Cavity Location  Combustion Efficiency  Tdlas  
Uncertainty in velocity measurement based on diode-laser absorption in nonuniform flows 期刊论文
APPLIED OPTICS, 2012, 卷号: 51, 期号: 20, 页码: 4788-4797
Authors:  Li F(李飞);  Yu XL(余西龙);  Cai WW;  Ma L;  Ma, L;  Virginia Tech, Dept Aerosp & Ocean Engn, Blacksburg, VA 24061 USA.
Adobe PDF(1161Kb)  |  Favorite  |  View/Download：920/290  |  Submit date：2013/01/18
Wavelength-modulation Spectroscopy  Water-vapor  Temperature Distributions  Scramjet Combustor  Gas Temperature  Parameters  Pressure  Sensors  
A compact sensor based on near infrared absorption spectroscopy for flow diagnostics in a low density hydrogen and oxygen combustion driven shock tube 期刊论文
Lasers in Engineering, 2012, 卷号: 23, 期号: 1-2, 页码: 1-17
Authors:  Yu XL(余西龙);  Li F(李飞);  Chen LH(陈立红);  Chang XY(张新宇)
Adobe PDF(1693Kb)  |  Favorite  |  View/Download：867/236  |  Submit date：2012/12/04
Tunable Diode-laser  Water-vapor  Scramjet Combustor  Temperature  Gases  H2o  Co  Oh  Tunable Diode Laser Absorption Spectroscopy (Tdlas)  Combustion  Rapid Time-division-multiplexing (Tdm)  Temperature  Water Vapour Concentration  Low Density Shock Tube  
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：1222/336  |  Submit date：2009/09/28
Scramjet  Combustor  Cavity  Performance