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Experimental investigation of mode transition process in a cavity-based scramjet 期刊论文
PHYSICS OF FLUIDS, 2024, 卷号: 36, 期号: 4, 页码: 11
Authors:  Meng Y(孟宇);  Sun WM(孙文明);  Gu HB(顾洪斌);  Chen, Fang
Favorite  |  View/Download：13/0  |  Submit date：2024/05/14
Supersonic Combustion Mode Analysis of a Cavity Based Scramjet 期刊论文
AEROSPACE, 2022, 卷号: 9, 期号: 12, 页码: 826
Authors:  Meng, Yu;  Sun WM(孙文明);  Gu HB(顾洪斌);  Chen, Fang;  Zhou RX(周芮旭)
Adobe PDF(3719Kb)  |  Favorite  |  View/Download：63/13  |  Submit date：2023/04/20
scramjet  combustion mode  POD  instability  
Experimental investigation of combustion-induced starting hysteresis in the scramjet 期刊论文
PHYSICS OF FLUIDS, 2022, 卷号: 34, 期号: 9, 页码: 96103
Authors:  Zhang QF(张启帆);  Chen H(陈昊);  Wu ZJ(吴振杰);  Gao ZB(高占彪);  Luo WH(罗苇航);  Gu HB(顾洪斌);  Yue LJ(岳连捷)
Adobe PDF(2852Kb)  |  Favorite  |  View/Download：170/56  |  Submit date：2022/10/23
Influence of Plasma on the Combustion Mode in a Scramjet 期刊论文
AEROSPACE, 2022, 卷号: 9, 期号: 2, 页码: 19
Authors:  Meng Y(孟宇);  Gu HB(顾洪斌);  Chen F(陈芳)
Adobe PDF(12588Kb)  |  Favorite  |  View/Download：175/45  |  Submit date：2022/05/17
scramjet  combustion  plasma  microwave  
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：1212/258  |  Submit date：2012/04/01
Absorption-spectroscopy  Water-vapor  Temperature Distributions  Gas Temperature  Combustion  Cavity  Operation  Engines  Model  
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