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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 [51]
李飞 [50]
余西龙 [40]
陈立红 [35]
顾洪斌 [18]
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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.
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Submit date:2015/06/12
Scramjet
Dual-mode Combustor
Divergent Angle
Cavity Location
Combustion Efficiency
Tdlas
双模态发动机的模态鉴别方法
期刊论文
力学学报, 2015, 期号: 3, 页码: 389-397
Authors:
李飞
;
王知溥
;
余西龙
;
顾洪斌
;
陈立红
;
张新宇
Adobe PDF(3140Kb)
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View/Download:423/74
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Submit date:2015/12/25
双模态冲压发动机
模态鉴别
释热分布
用于超燃诊断的吸收光谱二维诊断技术
会议论文
北京力学会第21届学术年会暨北京振动工程学会第22届学术年会, 中国北京, 2015-01-11
Authors:
李飞
;
余西龙
;
曾徽
;
张少华
;
顾洪斌
;
张新宇
Adobe PDF(737Kb)
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Submit date:2015/05/14
可调谐二极管吸收光谱技术(Tdlas)
二维断层成像术(Tdlat)
温度分布
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.
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Submit date:2014/12/18
双模态燃烧室构型对性能影响的实验研究
会议论文
第十六届全国激波与激波管学术会议, 中国河南洛阳, 2014-07-15
Authors:
王知溥
;
李飞
;
顾洪斌
;
余西龙
;
张新宇
Adobe PDF(1603Kb)
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Submit date:2015/07/01
双模态燃烧室
扩张角
凹腔
燃烧效率
吸收光谱
基于CN自由基的火星再入流场温度测量
期刊论文
力学学报, 2014, 卷号: 46, 期号: 2, 页码: 201-208
Authors:
林鑫
;
余西龙
;
李飞
;
张少华
;
辛建国
;
张新宇
Adobe PDF(818Kb)
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Submit date:2014/11/05
发射光谱
谱线强度
火星再入
转动温度
振动温度
基于TDLAS的层析成像技术TDLAT
期刊论文
力学学报, 2014, 期号: 1, 页码: 54-59
Authors:
李飞
;
余西龙
;
林鑫
;
张少华
;
张新宇
Adobe PDF(597Kb)
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Submit date:2014/11/05
可调谐二极管吸收光谱技术
二维断层成像术
温度分布
层析成像
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.
Adobe PDF(1235Kb)
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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)
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View/Download:1406/476
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Submit date:2013/05/03
Ethylene
Ignition
Numerical Simulation
Reduced Kinetic Mechanism
Supersonic Combustion
CO concentration and temperature measurements in a shock tube for Martian mixtures by coupling OES and TDLAS
期刊论文
APPLIED PHYSICS B-LASERS AND OPTICS, 2013, 卷号: 110, 期号: 3, 页码: 401-409
Authors:
Lin X(林鑫)
;
Yu XL(余西龙)
;
Li F(李飞)
;
Zhang SH(张少华)
;
Xin JG
;
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(716Kb)
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View/Download:1060/334
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Submit date:2013/04/16
Diode-laser Absorption
Nonequilibrium Radiation
Cn Radiation
Sensor
Entry
Flows
Wave