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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 [9]
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Numerical analysis on the heat transfer of three types of nozzles for the hypersonic long-run wind tunnel
期刊论文
Science China-Technological Sciences, 2015, 卷号: 58, 期号: 3, 页码: 470-475
Authors:
Xing YF(邢云绯)
;
Zhong FQ(仲峰泉)
;
Li DX(李东霞)
;
Zhang XY(张新宇)
;
Zhong, FQ (reprint author), Chinese Acad Sci, Inst Mech, Natl Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
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View/Download:466/204
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Submit date:2015/04/28
Hypersonic Scramjet Test Tunnel
Nozzle
Aerodynamic Heating
Convective Heat Transfer
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
Theoretical analysis of effects of boundary layer bleed on scramjet thrust
期刊论文
SCIENCE CHINA-PHYSICS MECHANICS & ASTRONOMY, 2013, 卷号: 56, 期号: 10, 页码: 1952-1961
Authors:
Yue LJ(岳连捷)
;
Xu XK(徐显坤)
;
Zhang XY(张新宇)
;
Yue, LJ (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:2013/10/23
Scramjet
Boundary Layer Bleed
Theoretical Analysis
Engine Thrust
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.
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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.
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Submit date:2013/05/03
Ethylene
Ignition
Numerical Simulation
Reduced Kinetic Mechanism
Supersonic Combustion
Effects of entry conditions on cracked kerosene-fueled supersonic combustor performance
期刊论文
Combustion Science and Technology, 2007, 卷号: 179, 期号: 10, 页码: 2199-2217
Authors:
Fan XJ(范学军)
;
Yu G(俞刚)
;
Li JG(李建国)
;
Yue LJ(岳连捷)
;
Zhang XY(张新宇)
;
Sung CJ
;
Fan, XJ (reprint author), Chinese Acad Sci, Inst Mech, Beijing 100080, Peoples R China.
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Submit date:2009/08/03
Entry Conditions
Kerosene
Supersonic Combustion
Thermal Cracking
Model Combustor
Propulsion
Injection
An Experimental Study of Kerosene Combustion in a Supersonic Model Combustor Using Effervescent Atomization
期刊论文
Proceedings of the Combustion Institute, 2005
Authors:
Yu G(俞刚)
;
Li JG(李建国)
;
Zhao JR(赵建荣)
;
Yue LJ(岳连捷)
;
Zhang XY(张新宇)
;
Sung CJ
;
Yu, G (reprint author), Chinese Acad Sci, Inst Mech, Beijing 100080, Peoples R China.
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Submit date:2007/06/15
Experimental Investigation on Flameholding Mechanism and Combustion Performance in Hydrogen-Fueled Supersonic Combustors
期刊论文
Combustion Science and Technology, 2002, 卷号: 174, 期号: 3, 页码: 1-27
Authors:
Yu G(俞刚)
;
Li JG(李建国)
;
Zhang XY(张新宇)
;
Chen LH(陈立红)
;
Han B
;
Sung CJ
;
Sung, CJ (reprint author), Case Western Reserve Univ, Dept Mech & Aerosp Engn, Cleveland, OH 44106 USA.
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Submit date:2007/06/15
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