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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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Ratified Gas Flows  Fokker-planck Equation  Langevin Simulation  Boundary Conditions  Stochastic Differential Equations  First Hitting Time  
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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Aerodynamic Coefficient  Data Correlation  Scaling Parameter  Genetic Programming  Invariant  
Preventing numerical oscillations in the flux-split based finite difference method for compressible flows with discontinuities 期刊论文
JOURNAL OF COMPUTATIONAL PHYSICS, 2015, 卷号: 300, 页码: 269-287
Authors:  He ZW;  Zhang YS;  Li XL(李新亮);  Li L;  Tian BL;  Tian, BL (reprint author), Inst Appl Phys & Computat Math, Lab Computat Phys, Beijing 100094, Peoples R China.
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Compressible Flows  Contact Discontinuity  Material Interface  Numerical Oscillations  Finite Difference Method  Flux Vector Splitting  Weno  
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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Supersonic Combustor  Convective Heat Transfer  Numerical Study  Wall Heat Flux  
A Slope Constrained 4th Order Multi-Moment Finite Volume Method with WENO Limiter 期刊论文
COMMUNICATIONS IN COMPUTATIONAL PHYSICS, 2015, 卷号: 18, 期号: 4, 页码: 901-930
Authors:  Sun ZY;  Teng HH(滕宏辉);  Xiao F;  Xiao, F (reprint author), Tokyo Inst Technol, Dept Energy Sci, Midori Ku, 4259 Nagatsuta, Yokohama, Kanagawa 2268502, Japan.
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Multi-moment Finite Volume Method  Weno  Flux Reconstruction  Compressible Flow  Conservative Method  Oscillation-suppressing  
Numerical study of oblique detonation wave initiation in a stoichiometric hydrogen-air mixture 期刊论文
PHYSICS OF FLUIDS, 2015, 卷号: 27, 期号: 9, 页码: 96101
Authors:  Wang T;  Zhang YN;  Teng HH(滕宏辉);  Jiang ZL(姜宗林);  Ng HD;  Wang, T (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
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An Algorithm for Calculating the RMS Value of the Non-Sinusoidal Current Used in AC Resistance Spot Welding 期刊论文
JOURNAL OF POWER ELECTRONICS, 2015, 卷号: 15, 期号: 4, 页码: 1139-1147
Authors:  Zhou K(周亢);  Cai, Lilong;  Zhou, K (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100080, Peoples R China.
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Model-independent  Neural Network  Nonlinear  Rms Value  Single-phase Ac Rsw  
Robust high-order space-time conservative schemes for solving conservation laws on hybrid meshes 期刊论文
JOURNAL OF COMPUTATIONAL PHYSICS, 2015, 卷号: 281, 页码: 375-402
Authors:  Shen H;  Wen CY;  Liu KX;  Zhang DL(张德良);  Shen, H (reprint author), Hong Kong Polytech Univ, Dept Mech Engn, Kowloon, Hong Kong, Peoples R China.
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Space-time Conservation Element And Solution Element (Ce/se) Method  High-order Accuracy  Hybrid Meshes  Unstructured Meshes  
Direct Numerical Simulation on Mach Number and Wall Temperature Effects in the Turbulent Flows of Flat-Plate Boundary Layer 期刊论文
COMMUNICATIONS IN COMPUTATIONAL PHYSICS, 2015, 卷号: 17, 期号: 1, 页码: 189-212
Authors:  Liang X;  Li XL(李新亮);  Li, XL (reprint author), Chinese Acad Sci, Inst Mech, LHD, 15 Beisihuanxi Rd, Beijing 100190, Peoples R China.
View  |  Adobe PDF(860Kb)  |  Favorite  |  View/Download：775/245  |  Submit date：2015/06/12
Hypersonic  Directly Numerical Simulation  Compressibility Effects  Turbulent Boundary Layer  Strong Reynolds Analogy