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中国科学院力学研究所机构知识库
Knowledge Management System of Institue of Mechanics, CAS
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张新宇 [5]
顾洪斌 [5]
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Indexed By:SCI
Creator:guhongbin分顾洪斌
Language:英语
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Experimental Study of Kerosene Ignition and Flame Stabilization in a Supersonic Combustor
期刊论文
International Journal of Turbo & Jet-Engines, 2022, 卷号: 39, 期号: 3, 页码: 403-410
Authors:
Meng Y(孟宇)
;
Gu HB(顾洪斌)
;
Zhang XY(张新宇)
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View/Download:247/84
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Submit date:2021/10/29
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
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)
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Adobe PDF(3099Kb)
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View/Download:371/98
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Submit date:2019/10/15
Scramjet Combustor Mode Transition Liquid Kerosene Acceleration
Experimental study of flame characteristics of ethylene and its mixture with methane and hydrogen in supersonic combustor
期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2019, 卷号: 86, 页码: 775-781
Authors:
Zhong FQ(仲峰泉)
;
Cheng LW(程柳维)
;
Gu HB(顾洪斌)
;
Zhang XY(张新宇)
Adobe PDF(2032Kb)
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View/Download:308/93
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Submit date:2019/05/29
Supersonic combustor
Hydrocarbon
Mixture fuel
Flame structure
Ignition
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
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View/Download:1204/258
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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)
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Adobe PDF(627Kb)
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View/Download:1174/323
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Submit date:2009/09/28
Scramjet
Combustor
Cavity
Performance