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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(1... [10]
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张新宇 [10]
岳连捷 [6]
俞刚 [5]
陈立红 [5]
Sung CJ [4]
李建国 [4]
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Creator:zhangxinyu分张新宇
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Design of Base Flow for Streamline-Traced Hypersonic Inlet
会议论文
16th AIAA/DLR/DGLR International Space Planes and Hypersonic Systems and Technologies Conference, International Space Planes and Hypersonic Systems and Technologies Conferences, Bremen, Germany, 19 October 2009 - 22 October 2009
Authors:
Yue LJ(岳连捷)
;
Xiao YB
;
Chen LH(陈立红)
;
Chang XY(张新宇)
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View/Download:221/87
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Submit date:2017/06/01
带中心支板侧压进气道流场特性研究
期刊论文
实验流体力学, 2008, 卷号: 22, 期号: 1, 页码: 31-35
Authors:
龚鹏
;
岳连捷
;
肖雅斌
;
王世芬
;
张新宇
Adobe PDF(621Kb)
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Submit date:2010/05/03
超燃冲压发动机
高超声速进气道
侧压式进气道
支板
Investigation on a truncated streamline-traced hypersonic Busemann inlet
会议论文
15th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, Dayton, OH, United states, April 28, 2008 - May 1, 2008
Authors:
Xiao YB(肖雅彬)
;
Yue LJ(岳连捷)
;
Gong P
;
Chang XY(张新宇)
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Adobe PDF(3472Kb)
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View/Download:215/85
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Submit date:2017/06/01
Boundary Layer Corrections
Busemann Inlet
Core Flow
Correction Method
Design Points
Finite Differential Methods
Internal Contraction Ratio
Internal Flows
Mass Flow
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
Research on three-dimensional scramjet inlet
会议论文
14th AIAA/AHI Space Planes and Hypersonic Systems and Technologies Conference, 2006, Beijing, China, 20-23 April 2006
Authors:
Yue LJ(岳连捷)
;
Xiao YB(肖雅彬)
;
Chen LH(陈立红)
;
Xiang AY(向安宇)
;
Zhang XY(张新宇)
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Submit date:2015/09/21
Research on three-dimensional scramiet inlet
会议论文
14th AIAA/AHI International Space Planes and Hypersonics Systems Technologies Conference, Canberra, Australia, November 6, 2006 - November 9, 2006
Authors:
Yue LJ(岳连捷)
;
Chen LH(陈立红)
;
Xiao YB
;
Gong P
;
Chang XY(张新宇)
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Adobe PDF(1267Kb)
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View/Download:151/51
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Submit date:2017/06/01
Capture Ratio
Mass Flow
Surface Oil Dot Visualization
Three-dimensional Scramjet Inlet
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
Adobe PDF(1024Kb)
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View/Download:1075/320
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Submit date:2007/12/18
Fuel Injection and Flame Stabilization in a Liquid-Kerosene-Fueled Supersonic Combustor
期刊论文
Journal of Propulsion and Power, 2003, 卷号: 19, 期号: 5, 页码: 885-893
Authors:
Yu G(俞刚)
;
Li JG(李建国)
;
Zhang XY(张新宇)
;
Chen LH(陈立红)
;
Sung CJ
;
Yu, G (reprint author), Chinese Acad Sci, Inst Mech, 15 Zhongguancun Rd, Beijing 100080, Peoples R China.
Adobe PDF(834Kb)
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View/Download:1050/414
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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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View/Download:724/220
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Submit date:2007/06/15
燃烧室构型对超燃冲压发动机性能影响研究
期刊论文
流体力学实验与测量, 2000, 卷号: 14, 期号: 1, 页码: 72
Authors:
俞刚
;
张新宇
Adobe PDF(418Kb)
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Submit date:2007/06/15
燃烧室构型
燃烧效率
总压损失
支板注射