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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... [4]
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张新宇 [6]
陈立红 [4]
俞刚 [2]
顾洪斌 [2]
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Creator:张新宇
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Document Type:会议论文
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Large eddy simulation of ignition and combustion of ethylene/air turbulent jet diffusion flame with reduced kinetic mechanism
会议论文
20th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, 2015, Glasgow, United kingdom, July 6, 2015 - July 9, 2015
Authors:
Ma SG(马素刚)
;
Zhong FQ(仲峰泉)
;
Zhang XY(张新宇)
;
Zhong, Fengquan (fzhong@imech.ac.cn)
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Submit date:2017/05/05
Combustion Pro
Cess
Directed Relation Graph
Dynamic Evolution
Fuel Injection Velocities
Kinetic Mechanism
Reduced Mechanisms
Temperature Profiles
Temporal And Spatial Evolutions
Study on Judgment Method of Combustion Mode on Dual-mode Scramjet
会议论文
7th Asian-Pacific Conference on Aerospace Technology and Science, 7th APCATS 2013, Taiwan, China, MAY 23-26, 2013
Authors:
Chen Q(陈强)
;
Chen LH(陈立红)
;
Gu HB(顾洪斌)
;
Zhang XY(张新宇)
;
Wang P
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Submit date:2014/03/11
Combustion Mode
Scramjet
Artificial Neural Network
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
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
Adobe PDF(519Kb)
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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