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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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Flow characteristic of highly underexpanded jets from various nozzle geometries
期刊论文
APPLIED THERMAL ENGINEERING, 2017, 卷号: 125, 页码: 240-253
Authors:
Li XP(李晓鹏)
;
Zhou, Rui
;
Yao W(姚卫)
;
Fan XJ(范学军)
;
Fan, XJ (reprint author), Chinese Acad Sci, State Key Lab High Temp Gas Dynam, Inst Mech, Beijing 100190, Peoples R China.
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View/Download:431/188
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Submit date:2017/11/16
Underexpanded Jets
Noncircular Jets
Nozzle Geometry
Large Eddy Simulation
Initiation structure of oblique detonation waves behind conical shocks
期刊论文
PHYSICS OF FLUIDS, 2017, 卷号: 29, 期号: 8
Authors:
Yang PF(杨鹏飞)
;
Ng, Hoi Dick
;
Teng HH(滕宏辉)
;
Jiang ZL(姜宗林)
;
Teng, HH (reprint author), Beijing Inst Technol, Sch Aerosp Engn, Dept Mech, Beijing 100081, Peoples R China.
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Submit date:2017/11/16
Numerical studies of shock wave interactions with a supersonic turbulent boundary layer in compression corner:Turning angle effects
期刊论文
COMPUTERS & FLUIDS, 2017, 卷号: 149, 页码: 56-69
Authors:
Tong FL(童福林)
;
Yu ZP(于长平)
;
Tang ZG(唐志共)
;
Li XL(李新亮)
;
Li, XL (reprint author), Chinese Acad Sci, Inst Mech, LHD, Beijing 100190, Peoples R China.
;
Li, XL (reprint author), Univ Chinese Acad Sci, Sch Engn Sci, Beijing 100049, Peoples R China.
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Submit date:2017/10/27
Compression Corner
Low-frequency Oscillation
Coherent Vortex Structure
Power Spectrum
Turbulent Kinetic Energy Budget
Direct Numerical Simulation
Molecular tagging velocimetry of NH fluorescence in a high-enthalpy rarefied gas flow
期刊论文
APPLIED PHYSICS B-LASERS AND OPTICS, 2017, 卷号: 123, 期号: 4
Authors:
Zhang SH(张少华)
;
Yu XL(余西龙)
;
Yan H
;
Huang HJ(黄河激)
;
Liu HL(刘宏立)
;
Yu, XL (reprint author), Chinese Acad Sci, Inst Mech, Beijing 100190, Peoples R China.
;
Yu, XL (reprint author), Univ Chinese Acad Sci, Sch Engn Sci, Beijing 100049, Peoples R China.
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Submit date:2017/07/24
Molecular Tagging Velocimetry
Nh Fluorescence
High-enthalpy
Rarefied Gas
Numerical investigation of characteristic frequency excited highly underexpanded jets
期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2017, 卷号: 63, 页码: 304-316
Authors:
Li XP
;
Fan E
;
Yao W(姚卫)
;
Fan XJ(范学军)
;
Fan, XJ (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
;
Fan, XJ (reprint author), Univ Chinese Acad Sci, Sch Engn Sci, Beijing 100049, Peoples R China.
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Submit date:2017/07/24
Fuel Jets
Underexpanded Jets
Jet Mixing Control
Excited Jets
Large Eddy Simulation
Numerical analysis of shock wave and supersonic turbulent boundary interaction between adiabatic and cold walls
期刊论文
JOURNAL OF TURBULENCE, 2017, 卷号: 18, 期号: 6, 页码: 569-588
Authors:
Tong, Fulin
;
Tang, Zhigong
;
Yu ZP(于长平)
;
Zhu, Xingkun
;
Li XL(李新亮)
;
Li, XL (reprint author), Chinese Acad Sci, Inst Mech, LHD, Beijing, Peoples R China.
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Submit date:2017/09/06
Shock Wave/turbulent Boundary Layer Interaction
Wall Temperature
Turbulence Structure
Shock Motion
Dynamic Mode Decomposition
Numerical Investigation on Flame Stabilization in DLR Hydrogen Supersonic Combustor with Strut Injection
期刊论文
COMBUSTION SCIENCE AND TECHNOLOGY, 2017, 卷号: 189, 期号: 12, 页码: 2154-2179
Authors:
Wu K(吴坤)
;
Zhang P(张鹏)
;
Yao W(姚卫)
;
Fan XJ(范学军)
;
Zhang, P (reprint author), Hong Kong Polytech Univ, Dept Mech Engn, Hong Kong 999077, Hong Kong, Peoples R China.
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Submit date:2017/12/18
Detailed Hydrogen Oxidation Mechanism
Dlr
Flame Stabilization
Sensitivity Analysis
Supersonic Combustion
Continuum perspective of bulk viscosity in compressible fluids
期刊论文
JOURNAL OF FLUID MECHANICS, 2017, 卷号: 812, 页码: 966-990
Authors:
Li XD
;
Hu ZM(胡宗民)
;
Jiang ZL(姜宗林)
;
Hu, ZM (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
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View/Download:442/148
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Submit date:2017/04/26
Direct numerical simulation of supersonic turbulent boundary layer subjected to a curved compression ramp
会议论文
Meeting of the Institute-of-Non-Newtonian-Fluid-Mechanics (INNFM), Llanwddyn, WALES, 2017
Authors:
Tong FL(童福林)
;
Li XL(李新亮)
;
Duan, Yanhui
;
Yu ZP(于长平)
;
Yu, CP (reprint author), Chinese Acad Sci, Inst Mech, LHD, Beijing 100190, Peoples R China.
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Submit date:2018/01/16
Concave Surface Curvature
Adverse Pressure-gradient
Large-eddy Simulation
Reynolds-number
Near-wall
Flows
Separation
Vortices
Models
Numerical Study on Wall Temperature Effects on Shock Wave/Turbulent Boundary-Layer Interaction
期刊论文
AIAA JOURNAL, 2017, 卷号: 55, 期号: 1, 页码: 131-140
Authors:
Zhu XK
;
Yu ZP(于长平)
;
Tong FL
;
Li XL(李新亮)
;
Li, 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:2017/04/26