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Indexed By:EI
Date Issued:2015
Language:英语
Community:高温气体动力学国家重点实验室
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An accurate treatment of diffuse reflection boundary conditions for a stochastic particle Fokker-Planck algorithm with large time steps
期刊论文
PHYSICA A-STATISTICAL MECHANICS AND ITS APPLICATIONS, 2015, 卷号: 440, 页码: 139-146
Authors:
Onskog T
;
Zhang J
;
Onskog, T (reprint author), KTH Royal Inst Technol, Dept Math, SE-10044 Stockholm, Sweden.
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Submit date:2016/01/08
Ratified Gas Flows
Fokker-planck Equation
Langevin Simulation
Boundary Conditions
Stochastic Differential Equations
First Hitting Time
Study on Flame Stabilization in a Dual-Mode Combustor Using Optical Measurements
期刊论文
JOURNAL OF PROPULSION AND POWER, 2015, 卷号: 31, 期号: 6, 页码: 1524-1531
Authors:
Yuan YM(袁越明)
;
Zhang TC(张泰昌)
;
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, 15 Beisihuanxi Rd, Beijing 100190, Peoples R China.
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Submit date:2016/03/21
Adaptive space transformation: An invariant based method for predicting aerodynamic coefficients of hypersonic vehicles
期刊论文
Engineering Applications of Artificial Intelligence, 2015, 卷号: 46, 页码: 93-103
Authors:
Luo CT(罗长童)
;
Hu ZM(胡宗民)
;
Zhang SL
;
Jiang ZL(姜宗林)
;
Luo, CT (reprint author), Chinese Acad Sci, Inst Mech, Beijing 100190, Peoples R China.
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Submit date:2016/01/07
Aerodynamic Coefficient
Data Correlation
Scaling Parameter
Genetic Programming
Invariant
A hybrid kinetic WENO scheme for inviscid and viscous flows
期刊论文
INTERNATIONAL JOURNAL FOR NUMERICAL METHODS IN FLUIDS, 2015, 卷号: 79, 期号: 6, 页码: 290-305
Authors:
Liu HW(刘洪伟)
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Submit date:2016/01/08
Weno Schemes
Kinetic Numerical Fluxes
Numerical Dissipations
Numerical study of combustion and convective heat transfer of a Mach 2.5 supersonic combustor
期刊论文
APPLIED THERMAL ENGINEERING, 2015, 卷号: 89, 页码: 883-896
Authors:
Wang X
;
Zhong FQ(仲峰泉)
;
Gu HB(顾宏斌)
;
Zhang XY(张新宇)
;
Zhong, FQ (reprint author), 15 Beisihuanxi Rd, Beijing 100190, Peoples R China.
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Submit date:2016/01/08
Supersonic Combustor
Convective Heat Transfer
Numerical Study
Wall Heat Flux
Aerothermal characteristics of bleed slot in hypersonic flows
期刊论文
SCIENCE CHINA-PHYSICS MECHANICS & ASTRONOMY, 2015, 卷号: 58, 期号: 10, 页码: 104703
Authors:
Yue LJ(岳连捷)
;
Lu HB
;
Xu X
;
Chang XY
;
Yue, LJ (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:2016/01/08
Boundary Layer Control
Boundary Layer Heat Flow
Shock Wave Interactions
Separated Flows
Improvement of weighted compact scheme with multi-step strategy for supersonic compressible flow
期刊论文
COMPUTERS & FLUIDS, 2015, 卷号: 115, 页码: 2841-2849
Authors:
Peng J(彭峻)
;
Shen YQ(申义庆)
;
Shen, YQ (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:2016/01/08
Numerical Method
Supersonic Compressible Flow
Weighted Compact Scheme
Multi-step Strategy
Experimental study on convection heat transfer and air drag in sinter layer
期刊论文
JOURNAL OF CENTRAL SOUTH UNIVERSITY, 2015, 卷号: 22, 期号: 7, 页码: 2841-2848
Authors:
Pan LS(潘利生)
;
Wei XL(魏小林)
;
Peng Y
;
Shi XB
;
Liu HL
;
Pan, LS (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:2015/10/21
Sinter Layer
Convection Heat Transfer
Pressure Drop
Development and Preliminary Validation of A Thermal Analysis Method for Hydrocarbon Regenerative-cooled Supersonic Combustor
会议论文
20th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, Glasgow, Scotland, 6-9 July, 2015
Authors:
Lu Y(陆阳)
;
Wang XZ(王新竹)
;
Li L(李龙)
;
Cheng D(程迪)
;
Yuan T(袁涛)
;
Yao W(姚卫)
;
Fan XJ(范学军)
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Submit date:2016/01/08
Hydrocarbons
Combustors
Cooling
Heat Transfer
Numerical study of heat transfer deterioration of turbulent supercritical kerosene flow in heated circular tube
期刊论文
INTERNATIONAL JOURNAL OF HEAT AND MASS TRANSFER, 2015, 卷号: 85, 页码: 1003-1011
Authors:
Dang GX
;
Zhong FQ(仲峰泉)
;
Zhang YJ
;
Zhang XY(张新宇)
;
Zhong, FQ (reprint author), Chinese Acad Sci, Inst Mech, Bei Si Huan Xi Rd 15, Beijing 100190, Peoples R China.
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Submit date:2015/06/12
Supercritical Kerosene
Convective Heat Transfer
Turbulent Flow
Numerical Study