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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 [11]
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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
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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View/Download:566/234
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Submit date:2015/06/12
Scramjet
Dual-mode Combustor
Divergent Angle
Cavity Location
Combustion Efficiency
Tdlas
Experimental study of combustion oscillations in a dual-mode scramjet
会议论文
20th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, 2015, 2015
Authors:
Tian XD
;
Chen LH(陈立红)
;
Gu HB(顾洪斌)
;
Liu C
;
Cheng LW
;
Chang XY(张新宇)
;
Chen, Lihong (lhchen@imech.ac.cn)
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Submit date:2017/09/04
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.
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View/Download:1443/494
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Submit date:2013/05/03
Ethylene
Ignition
Numerical Simulation
Reduced Kinetic Mechanism
Supersonic Combustion
用DDES方法对凹腔火焰稳定的研究
会议论文
LHD2011夏季学术研讨会, 内蒙赤峰, 2011
Authors:
郭帅帅
;
万田
;
陈立红
;
张新宇
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Submit date:2014/01/23
凹腔
燃烧
火焰稳定机理
激波剪切层相互作用
Ddes
模型
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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View/Download:1184/328
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Submit date:2009/09/28
Scramjet
Combustor
Cavity
Performance
超声速燃烧室凹腔火焰稳定器的数值模拟
期刊论文
推进技术, 2007, 卷号: 28, 期号: 2, 页码: 135-140
Authors:
陈方
;
陈立红
;
张新宇
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Submit date:2010/05/03
超音速燃烧
凹体
燃烧性能
氢
数值仿真
壁面凹腔强化H2超声速燃烧的数值模拟
期刊论文
推进技术, 2006, 期号: 6, 页码: 563-567
Authors:
陈方
;
陈立红
;
张新宇
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Submit date:2007/06/15
Investigation of Vaporized Kerosene Injection and Combustion in a Supersonic Model Combustor
会议论文
AIAA/ASME/SAE/ASEE 40th Joint Propulsion Conference
Authors:
Fan XJ(范学军)
;
Yu G(俞刚)
;
Li JG(李建国)
;
Zhang XY(张新宇)
;
Sung CJ
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View/Download:1091/329
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Submit date:2007/12/18
Investigation of kerosene combustion characteristics with pilot hydrogen in model supersonic combustors
期刊论文
Journal of Propulsion and Power, 2001, 卷号: 17, 期号: 6, 页码: 1263-1272
Authors:
Yu G(俞刚)
;
Li JG(李建国)
;
Zhang XY(张新宇)
;
Chen LH(陈立红)
;
Song CJ
;
Yu, G (reprint author), Chinese Acad Sci, Inst Mech, 15 Zhongguancun Rd,Haidian Dist, Beijing 100080, Peoples R China.
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Submit date:2007/06/15