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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... [5]
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张新宇 [9]
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Indexed By:EI
Creator:张新宇
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Document Type:会议论文
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The Phenomena of Sudden Change in Hypersonic Inlets Self-Starting Capability
会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017
Authors:
Jia YN(贾轶南)
;
Yue LJ(岳连捷)
;
Zhang XY(张新宇)
;
Jia, Yinan(yuelj@imech.ac.cn)
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Submit date:2018/01/16
Boundary Layer Flow
Boundary Layers
Spacecraft
Wind Tunnels
Combined TDLAS and OES technique for CO concentration measurement in shock-heated Martian atmosphere
会议论文
2nd International Symposium on Laser Interaction with Matter (LIMIS), Xian, PEOPLES R CHINA, SEP 09-12, 2012
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.
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Submit date:2013/12/12
Optical Emission Spectroscopy (Oes)
Tunable Diode Laser Absorption Spectroscopy (Tdlas)
Shock Wave
Temperature
Concentration
Measurement of temperature, velocity and water vapor concentration in a scramjet combustor based on nearinfrared diode laser absorption
会议论文
17th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, San Francisco, CA, United states, APR 11-14, 2011
Authors:
Li F(李飞)
;
Yu XL(余西龙)
;
Gu HB(顾洪斌)
;
Li Z(李智)
;
Chen LH(陈立红)
;
Zhang XY(张新宇)
;
Li F(李飞)
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Submit date:2014/02/24
Characteristics of supersonic combustion with Hartmann-Sprenger tube aided fuel injection
会议论文
17th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, San Francisco, CA, United states, APR 11-14, 2011
Authors:
Gu HB(顾洪斌)
;
Li Z(李智)
;
Li F(李飞)
;
Chen LH(陈立红)
;
Gu SL(顾声龙)
;
Zhang XY(张新宇)
;
Gu HB(顾洪斌)
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Submit date:2014/02/24
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
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