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Parallel computing strategy for a flow solver based on immersed boundary method and discrete stream-function formulation 期刊论文
COMPUTERS & FLUIDS, 2013, 卷号: 88, 页码: 210-224
Authors:  Wang SZ(王士召);  He GW(何国威);  Zhang X(张星);  Zhang, X (reprint author), Chinese Acad Sci, Inst Mech, LNM, Beijing 100190, Peoples R China.
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Parallelization  Domain Decomposition  Massage Passing Interface  Immersed Boundary Method  Discrete Stream-function Formulation  
A comparative study of truly incompressible and weakly compressible SPH methods for free surface incompressible flows 期刊论文
INTERNATIONAL JOURNAL FOR NUMERICAL METHODS IN FLUIDS, 2013, 卷号: 73, 期号: 9, 页码: 813-829
Authors:  Chen Z;  Zong Z;  Liu MB(刘谋斌);  Li HT;  Liu, MB (reprint author), Chinese Acad Sci, Inst Mech, Key Lab Mech Fluid Solid Coupling Syst, Beijing 100190, Peoples R China.
Adobe PDF(2150Kb)  |  Favorite  |  View/Download:870/349  |  Submit date:2013/11/06
Incompressible Sph  Weakly Compressible Sph  Free Surface Flows  Fluid-structure Interaction  
Optimized sixth-order monotonicity-preserving scheme by nonlinear spectral analysis 期刊论文
INTERNATIONAL JOURNAL FOR NUMERICAL METHODS IN FLUIDS, 2013, 卷号: 73, 期号: 6, 页码: 560–577
Authors:  Li XL(李新亮);  Leng Y(冷岩);  He ZW(何志伟);  Li, XL (reprint author), Chinese Acad Sci, LHD Inst Mech, Beijing 100190, Peoples R China
Adobe PDF(1159Kb)  |  Favorite  |  View/Download:1121/435  |  Submit date:2013/09/21
Nonlinear Spectral Analysis  Monotonicity-preserving  Optimization  Shock-capturing Schemes  Dissipation  Dispersion  
Towards an entropy-based detached-eddy simulation 期刊论文
SCIENCE CHINA-PHYSICS MECHANICS & ASTRONOMY, 2013, 卷号: 56, 期号: 10, 页码: 1970-1980
Authors:  Zhao R(赵瑞);  Yan C(阎超);  Li XL(李新亮);  Kong WX;  Zhao, R (reprint author), Beijing Univ Aeronaut & Astronaut, Natl Lab Computat Fluid Dynam, Beijing 100191, Peoples R China.
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Hybrid Rans/les  Detached-eddy Simulation  Turbulence  Compressible Flows  Entropy  
Conceptual design and aerodynamic evaluation of hypersonic airplane with double flanking air inlets 期刊论文
SCIENCE CHINA-TECHNOLOGICAL SCIENCES, 2013, 卷号: 56, 期号: 8, 页码: 1980-1988
Authors:  Cui K(崔凯);  Hu SC(胡守超);  Li GL(李广利);  Qu ZP(屈志朋);  Situ M;  Cui, K (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
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Hypersonic  Flanking Air Inlet  Waverider  Computational Fluid Dynamics(Cfd)  
Improvement of Baldwin-Lomax turbulence model for supersonic complex flows 期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2013, 卷号: 26, 期号: 3, 页码: 529–534
Authors:  Zhao R(赵瑞);  Yan C(阎超);  Yu J(于剑);  Li XL(李新亮);  Yan, C (reprint author), Beihang Univ, Sch Aeronaut Sci & Engn, Beijing 100191, Peoples R China.
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Baldwin-lomax Model  Boundary Layers  Computational Aerodynamics  Entropy  Supersonic Flows  Turbulence Models  
Numerical simulation of ignition and combustion of ethylene in a supersonic model combustor with a reduced kinetic mechanism 期刊论文
COMBUSTION SCIENCE AND TECHNOLOGY, 2013, 卷号: 185, 期号: 4, 页码: 548-563
Authors:  Zhong FQ(仲峰泉);  Chen LH(陈立红);  Li F(李飞);  Zhang XY(张新宇);  Sung CJ;  Zhong, FQ (reprint author), Chinese Acad Sci, State Key Lab High Temp Gas Dynam, Inst Mech, Beijing 100190, Peoples R China.
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Ethylene  Ignition  Numerical Simulation  Reduced Kinetic Mechanism  Supersonic Combustion  
A reconstructed discontinuous Galerkin method based on a Hierarchical WENO reconstruction for compressible flows on tetrahedral grids 期刊论文
JOURNAL OF COMPUTATIONAL PHYSICS, 2013, 卷号: 236, 页码: 477-492
Authors:  Luo H;  Xia YD;  Spiegel S;  Nourgaliev R;  Jiang ZL(姜宗林);  Luo, H (reprint author), N Carolina State Univ, Dept Mech & Aerosp Engn, Raleigh, NC 27695 USA.
Adobe PDF(2739Kb)  |  Favorite  |  View/Download:1398/509  |  Submit date:2013/03/25
Discontinuous Galerkin Method  Weno Reconstruction  Unstructured Grids  
Flutter analyses of complete aircraft based on hybrid grids and parallel computing 期刊论文
SCIENCE CHINA-TECHNOLOGICAL SCIENCES, 2013, 卷号: 56, 期号: 2, 页码: 398-404
Authors:  Zheng GN(郑冠男);  Yang GW(杨国伟);  Qian W;  Yang, GW (reprint author), Chinese Acad Sci, Inst Mech, Key Lab Mech Fluid Solid Coupling Syst, Beijing 100190, Peoples R China.
Adobe PDF(4121Kb)  |  Favorite  |  View/Download:994/220  |  Submit date:2013/03/25
Cfd  Csd  Aeroelasticity  Coupled Method  Flutter  Mpi  
Detailed modeling of the effects of K/Na additives on the thermal DeNO(x) process 期刊论文
ENERGY & FUELS, 2013, 卷号: 27, 期号: 1, 页码: 421-429
Authors:  Guo XF(郭啸峰);  Wei XL(魏小林);  Li S(李森);  Wei, XL (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
Adobe PDF(628Kb)  |  Favorite  |  View/Download:1314/381  |  Submit date:2013/05/21
Computational Fluid Dynamics  Experiments  Oxygen  Potassium  Selective Catalytic Reduction  Sodium  Chemistry Mechanism  Detailed Chemical Kinetic  Detailed Modeling  Entrained Flow Reactor  Metal Additives  Na Concentration  No Reduction  Normalized Stoichiometric Ratio  Oxygen Concentrations  Promoting Effect  Radical Production  Reduced Mechanisms  Selective Non-catalytic Reduction  Sodium Additive  Temperature Range  Temperature Window  Thermal Deno