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关于二平行流束之间层流边界层流动方程式的解
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作者 李心铭 李臻 《海洋通报》 CAS CSCD 北大核心 1999年第1期18-27,共10页
通过选取一以两层流束分界面上的流体速度平动的坐标系,证明两流束中的层流边界层流动可以劈分为两个与沿平板的边界层流动完全相同的流动并且应用已有的沿平板边界层流动的精确解,可以给出具有不同密度、不同粘性与不同速度的二平行流... 通过选取一以两层流束分界面上的流体速度平动的坐标系,证明两流束中的层流边界层流动可以劈分为两个与沿平板的边界层流动完全相同的流动并且应用已有的沿平板边界层流动的精确解,可以给出具有不同密度、不同粘性与不同速度的二平行流束之间层流边界层流动方程式的精确解.就Lock讨论的情况,应用本文提出的方法所得到的结果跟Lock所作的数值计算作了详细的比较. 展开更多
关键词 边界层 平行流束 Blasius解 流动方程式
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UPWIND SCHEME FOR IDEAL 2-D MHD FLOWS BASED ON UNSTRUCTURED MESH 被引量:1
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作者 潘勇 王江峰 伍贻兆 《Transactions of Nanjing University of Aeronautics and Astronautics》 EI 2007年第1期1-7,共7页
An upwind scheme based on the unstructured mesh is developed to solve ideal 2-D magnetohydrodynamics (MHD) equations. The inviscid fluxes are approximated by using the modified advection upstream splitting method (... An upwind scheme based on the unstructured mesh is developed to solve ideal 2-D magnetohydrodynamics (MHD) equations. The inviscid fluxes are approximated by using the modified advection upstream splitting method (AUSM) scheme, and a 5-stage explicit Runge-Kutta scheme is adopted in the time integration. To avoid the influence of the magnetic field divergence created during the simulation, the hyperbolic divergence cleaning method is introduced. The shock-capturing properties of the method are verified by solving the MHD shock-tube problem. Then the 2-D nozzle flow with the magnetic field is numerically simulated on the unstructured mesh. Computational results demonstrate the effects of the magnetic field and agree well with those from references. 展开更多
关键词 ideal magnetohydrodynamics equation unstructured mesh advection upstream splitting method(AUSM) scheme divergence cleaning
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A General Formula of Flow Equations for Harry-Dym Hierarchy
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作者 程纪鹏 贺劲松 王立洪 《Communications in Theoretical Physics》 SCIE CAS CSCD 2011年第2期193-198,共6页
In this paper, we derive a general formula of the flow equtions for the Harry-Dym hierarchy. And three applications in n-reduction, (2 + 1)-dimensional generalization, and Kupershmidt reduction, are considered.
关键词 Harry-Dym equation Harry-Dym hierarchy Lax equation flow equations
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On Recursion Operator of the q-KP Hierarchy 被引量:1
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作者 田可雷 朱晓鸣 贺劲松 《Communications in Theoretical Physics》 SCIE CAS CSCD 2016年第9期263-268,共6页
It is the aim of the present article to give a general expression of flow equations of the q-KP hierarchy.The distinct difference between the q-KP hierarchy and the KP hierarchy is due to q-binomial and the action of ... It is the aim of the present article to give a general expression of flow equations of the q-KP hierarchy.The distinct difference between the q-KP hierarchy and the KP hierarchy is due to q-binomial and the action of q-shift operator θ, which originates from the Leibnitz rule of the quantum calculus. We further show that the n-reduction leads to a recursive scheme for these flow equations. The recursion operator for the flow equations of the q-KP hierarchy under the n-reduction is also derived. 展开更多
关键词 q-KP hierarchy flow equations recursion operator
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A semi-implicit three-step method based on SUPG finite element formulation for flow in lid driven cavities with different geometries 被引量:1
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作者 Cheng HUAN Dai ZHOU Yan BAO 《Journal of Zhejiang University-Science A(Applied Physics & Engineering)》 SCIE EI CAS CSCD 2011年第1期33-45,共13页
A numerical algorithm using a bilinear or linear finite element and semi-implicit three-step method is presented for the analysis of incompressible viscous fluid problems. The streamline upwind/Petrov-Galerkin (SUPG) ... A numerical algorithm using a bilinear or linear finite element and semi-implicit three-step method is presented for the analysis of incompressible viscous fluid problems. The streamline upwind/Petrov-Galerkin (SUPG) stabilization scheme is used for the formulation of the Navier-Stokes equations. For the spatial discretization, the convection term is treated explicitly, while the viscous term is treated implicitly, and for the temporal discretization, a three-step method is employed. The present method is applied to simulate the lid driven cavity problems with different geometries at low and high Reynolds numbers. The results compared with other numerical experiments are found to be feasible and satisfactory. 展开更多
关键词 Semi-implicit three-step method Streamline upwind/Petrov-Galerkin (SUPG) finite element method (FEM) Unsteady incompressible flows Lid driven cavity problem
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Implementation of the moving particle semi-implicit method on GPU 被引量:2
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作者 ZHU XiaoSong CHENG Liang +1 位作者 LU Lin TENG Bin 《Science China(Physics,Mechanics & Astronomy)》 SCIE EI CAS 2011年第3期523-532,共10页
The Moving Particle Semi-implicit (MPS) method performs well in simulating violent free surface flow and hence becomes popular in the area of fluid flow simulation. However, the implementations of searching neighbouri... The Moving Particle Semi-implicit (MPS) method performs well in simulating violent free surface flow and hence becomes popular in the area of fluid flow simulation. However, the implementations of searching neighbouring particles and solving the large sparse matrix equations (Poisson-type equation) are very time-consuming. In order to utilize the tremendous power of parallel computation of Graphics Processing Units (GPU), this study has developed a GPU-based MPS model employing the Compute Unified Device Architecture (CUDA) on NVIDIA GTX 280. The efficient neighbourhood particle searching is done through an indirect method and the Poisson-type pressure equation is solved by the Bi-Conjugate Gradient (BiCG) method. Four different optimization levels for the present general parallel GPU-based MPS model are demonstrated. In addition, the elaborate optimization of GPU code is also discussed. A benchmark problem of dam-breaking flow is simulated using both codes of the present GPU-based MPS and the original CPU-based MPS. The comparisons between them show that the GPU-based MPS model outperforms 26 times the traditional CPU model. 展开更多
关键词 moving particle semi-implicit method (MPS) graphics processing units (GPU) compute unified device architecture (CUDA) neighbouring particle searching free surface flow
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