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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... [6]
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张新宇 [6]
俞刚 [4]
陈立红 [3]
李建国 [2]
Huang QS [1]
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Indexed By:EI
Creator:张新宇
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A tunable diode-laser absorption spectroscopy (TDLAS) thermometry for combustion diagnostics
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:
Yu XL(余西龙)
;
Li F(李飞)
;
Chen LH(陈立红)
;
Chang XY(张新宇)
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Submit date:2017/06/01
Absorption Lines
Combustion Diagnostics
Direct Absorption
Fiber-coupled
Flat Flame Burner
High Sensitivity
Near Infrared
Non-intrusive
Premixed
Scan Rates
Thermocouple Measurements
Tunable Diode Laser Absorption Spectroscopy
Tunable Diode Lasers
Water Vapor Concentration
Water-vapor Absorption
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
Analyses of supersonic combustion by gas sampling
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:
Chen LH(陈立红)
;
Lin R
;
Gu HB(顾洪斌)
;
Chang XY(张新宇)
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Submit date:2017/06/01
Combustion Efficiency
Gas Sampling
Probe Sampling
Scramjet
Planar Laser induced Fluorescence Imaging of OH Radical in Supersonic Combustor
会议论文
Conference on Optical Technology and Image Processing for Fluids and Solids Diagnostics 2002, BEIJING, PEOPLES R CHINA, SEP 03-06, 2002
Authors:
Yang SR(杨仕润)
;
Zhao JR(赵建荣)
;
Yu G(俞刚)
;
Zhang XY(张新宇)
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Submit date:2007/06/15
Development of the facility for model scramjet testing
会议论文
10th AIAA/NAL-NASDA-ISAS International Space Planes and Hypersonic Systems and Technologies Conference 2001, Kyoto, Japan, April 24, 2001 - April 27, 2001
Authors:
Chang XY(张新宇)
;
Chen LH(陈立红)
;
Yu G(俞刚)
;
Qian DX(钱大兴)
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Submit date:2017/06/01
Chinese Academy Of Sciences
Enthalpy Flow
Hypersonic Propulsion Test Facility
Performance Tests
Scramjet Testing
Supersonic Combustion
Total Pressure
Total Temperatures
Combustion of kerosene in a supersonic stream
会议论文
38th Aerospace Sciences Meeting and Exhibit 2000, Reno, NV, United states, January 10, 2000 - January 13, 2000
Authors:
Li JG(李建国)
;
Yu G(俞刚)
;
Zhang XY(张新宇)
;
Huang QS
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Submit date:2017/06/01
Cavity Flame Holders
Combustion Efficiencies
Combustor Performance
Equivalence Ratios
Modular Structures
Optimized Conditions
Stagnation Pressures
Supersonic Combustors