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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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力学所知识产出(19... [1]
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张新宇 [8]
顾洪斌 [8]
陈立红 [4]
孟宇 [3]
孙文明 [2]
李智 [2]
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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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Submit date:2021/10/29
微波增强滑移电弧等离子体辅助超声速燃烧
期刊论文
航空学报, 2020, 卷号: 41, 期号: 2, 页码: 123345
Authors:
孟宇
;
顾洪斌
;
孙文明
;
张新宇
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Submit date:2019/12/16
超燃冲压发动机
超声速燃烧
等离子体助燃
滑移电弧
微波
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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Submit date:2019/10/15
Scramjet Combustor Mode Transition Liquid Kerosene Acceleration
CH* Luminance Distribution Application and a One-Dimensional Model of the Supersonic Combustor Heat Release Quantization
期刊论文
INTERNATIONAL JOURNAL OF TURBO & JET-ENGINES, 2019, 卷号: 36, 期号: 1, 页码: 45-50
Authors:
Wang ZP(王知溥)
;
Gu HB(顾洪斌)
;
Cheng L W
;
Zhong FQ(仲峰泉)
;
Zhang XY(张新宇)
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Submit date:2019/04/11
supersonic combustion
one-dimensional modelling
heat release
CH* chemiluminescence
乙烯燃料双模态燃烧室模态转换影响参数研究
会议论文
第四届高超声速科技学术会议, 中国海南三亚, 2011
Authors:
李珊珊
;
顾洪斌
;
陈强
;
李智
;
陈立红
;
张新宇
Adobe PDF(70Kb)
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Submit date:2012/04/01
双模态
燃烧室
乙烯燃料
调节范围
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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Submit date:2012/04/01
Absorption-spectroscopy
Water-vapor
Temperature Distributions
Gas Temperature
Combustion
Cavity
Operation
Engines
Model
污染空气效应对乙烯燃料超燃冲压发动机燃烧室流场影响的数值评估
会议论文
第三届高超声速科技学术会议会议, 中国江苏无锡, 2010-10-26
Authors:
万田
;
顾洪斌
;
陈立红
;
张新宇
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Submit date:2014/04/02
污染空气
数值模拟
乙烯
超燃冲压发动机
燃烧室
Thrust and drag of a scramjet model with different combustor geometries
会议论文
13th AIAA/CIRA International Space Planes and Hypersonic Systems and Technologies Conference, Capua, Italy, May 16, 2005 - May 20, 2005
Authors:
Chang XY(张新宇)
;
Gu HB(顾洪斌)
;
Chen LH(陈立红)
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Submit date:2017/06/01
Combustor Geometries
Flame Stabilization
Mixing Enhancement
Scramjets