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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... [8]
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reprint au... [4]
傅德薰 [3]
李新亮 [3]
马延文 [3]
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Date Issued:2008
Language:英语
Community:力学所知识产出(1956-2008)
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Numerical study of the oscillations induced by shock/shock interaction in hypersonic double-wedge flows
期刊论文
SHOCK WAVES, 2008, 卷号: 18, 期号: 1, 页码: 41-51
Authors:
Hu ZM(胡宗民)
;
Myong R S
;
Wang C(王春)
;
Cho T H
;
Jiang ZL(姜宗林)
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View/Download:215/87
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Submit date:2020/08/26
Shock
Shock Interaction
Oscillation
Hypersonic
Double-wedge
Numerical Study
Receptivity To Free-Stream Disturbance Waves For Hypersonic Flow Over A Blunt Cone
期刊论文
Science In China Series G-Physics Mechanics & Astronomy, 2008, 页码: 1682-1690
Authors:
Zhang YD(张玉东)
;
Fu DX(傅德薰)
;
Ma YW(马延文)
;
Li XL(李新亮)
;
Zhang, YD (reprint author), China Acad Aerosp Aerodynam, Beijing 100074, Peoples R China.
Adobe PDF(265Kb)
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View/Download:913/199
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Submit date:2009/08/03
Receptivity
Research Progress On Thermal Protection Materials And Structures Of Hypersonic Vehicles
期刊论文
Applied Mathematics and Mechanics (English Edition), 2008, 页码: 51-60
Authors:
Yang YZ(杨亚政)
;
Yang JL
;
Fang DN
;
Yang, YZ (reprint author), Beijing Univ Aeronaut & Astronaut, Sch Aeronaut Sci & Technol, Beijing 100083, Peoples R China.
Adobe PDF(601Kb)
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View/Download:934/366
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Submit date:2009/08/03
Hypersonic Vehicle
High-temperature
Thermal Protection
High-temperature Ceramics
Carbon/carbon Composites
Oxidation Behavior
Creep-behavior
Carbon
Microstructure
Diboride
Kinetics
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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View/Download:216/85
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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
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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Adobe PDF(265Kb)
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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
Dns Of Compressible Turbulent Boundary Layer Around A Sharp Cone
期刊论文
Science In China Series G-Physics Mechanics & Astronomy, 2008, 页码: 699-714
Authors:
Li XL(李新亮)
;
Fu DX(傅德薰)
;
Ma YW(马延文)
;
Li, XL (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab Nonlinear Mech, Beijing 100080, Peoples R China.
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Submit date:2009/08/03
Direct Numerical Simulation
New trends in fluid mechanics research : proceeding of the fifth international conference on fluid mechanics (Shanghai, 2007)
专著
Beijing : New York:Tsinghua Univ. Press, Springer, 2008
Authors:
editors, 庄逢甘
;
Li JC(李家春)
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View/Download:1213/29
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Submit date:2009/07/06
Direct Numerical Simulation Of Hypersonic Boundary-Layer Transition Over A Blunt Cone
期刊论文
AIAA Journal, 2008, 页码: 2899-2913
Authors:
Li XL(李新亮)
;
Fu DX(傅德薰)
;
Ma YW(马延文)
;
Li, XL (reprint author), Chinese Acad Sci, Inst Mech, Lab Nonlinear Mech, Beijing 100080, Peoples R China.
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Submit date:2009/08/03
Hyperbolic Conservation-laws