共查询到20条相似文献,搜索用时 93 毫秒
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本文介绍了基于边的数据结果离散对流扩散方程的方法,编制了适用于任意多边形单元网格的有限容积法计算程序,利用方腔自然对流、外掠后台阶和移动顶盖驱等算例考察了三角形网格与多边形网格在数值计算方面的性能差别.结果表明,采用三角形网格收敛较慢且不容易获得网格无关的解,而采用与三角形网格对偶的多边形网格则收敛较快且易获得网格无关的解. 相似文献
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结合前沿推进的Delaunay三角化网格生成及应用 总被引:4,自引:3,他引:1
采用一种新的混合网格生成方法,生成复杂区域的非结构化网格.结合前沿推进法和Delaunay三角化两种非结构网格生成方法的特点,在边界处采用前沿推进法进行三角形初始网格的生成,在边界区域内部采用Delaunay三角化方法自动生成内部节点.分析表明,该算法简化网格生成过程,能够快速有效地生成非结构化网格.在计算时间以及网格的均匀性方面与其他方法相比具有一定的优势.最后,用混合网格生成方法生成方柱绕流的计算域网格,并运用基于特征线方程的分离算法进行流场计算. 相似文献
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研究自适应Runge-Kutta间断Galerkin (RKDG)方法求解双曲守恒律方程组,并提出两种生成相容三角形网格的自适应算法.第一种算法适用于规则网格,实现简单、计算速度快.第二种算法基于非结构网格,设计一类基于间断界面的自适应网格加密策略,方法灵活高效.两种方法都具有令人满意的计算效果,而且降低了RKDG的计算量. 相似文献
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Unstructured meshes are in widespread use throughout computational physics, but calculating diagnostics of simulations on such meshes can be challenging. For example, in geophysical fluid dynamics, it is frequently desirable to compute directional integrals such as vertical integrals and zonal averages; however, it is difficult to compute these on meshes with no inherent spatial structure. This is widely regarded as an obstacle to the adoption of unstructured mesh numerical modelling in this field. In this paper, we describe an algorithm by which one can exactly compute such directional integrals on arbitrarily unstructured meshes. This is achieved via the solution of a problem of computational geometry, constructing the supermesh of two meshes. We demonstrate the utility of this approach by applying it to a classical geophysical fluid dynamics system: the thermally driven rotating annulus. This addresses an important objection to the more widespread use of unstructured mesh modelling. 相似文献
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利用流体力学方程的积分形式给出非结构移动网格上离散格式,利用自适应移动网格方法移动网格,进而得到网格速度.对振动Naca0012翼型问题,分三种类型确定网格速度,再结合Riemann问题的解法器构造数值通量,得到移动网格单元上新的物理量.数值实验表明这种格式同时具有高效、高分辨率的特点. 相似文献
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将龙格库塔间断有限元方法(RDDG)与自适应方法相结合,求解三维欧拉方程.区域剖分采用非结构四面体网格,依据数值解的变化采用自适应技术对网格进行局部加密或粗化,减少总体网格数目,提高计算效率.给出四种自适应策略并分析不同自适应策略的优缺点.数值算例表明方法的有效性. 相似文献
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Reduction of Numerical Oscillations in Simulating Moving-Boundary Problems by the Local DFD Method 下载免费PDF全文
In this work, the hybrid solution reconstruction formulation proposed by
Luo et al. [H. Luo, H. Dai, P. F. de Sousa and B. Yin, On the numerical oscillation of the
direct-forcing immersed-boundary method for moving boundaries, Computers & Fluids,
56 (2012), pp. 61–76] for the finite-difference discretization on Cartesian meshes
is implemented in the finite-element framework of the local domain-free discretization
(DFD) method to reduce the numerical oscillations in the simulation of moving-boundary
flows. The reconstruction formulation is applied at fluid nodes in the immediate
vicinity of the immersed boundary, which combines weightly the local DFD
solution with the specific values obtained via an approximation of quadratic polynomial
in the normal direction to the wall. The quadratic approximation is associated
with the no-slip boundary condition and the local simplified momentum equation.
The weighted factor suitable for unstructured triangular and tetrahedral meshes is
constructed, which is related to the local mesh intervals near the immersed boundary
and the distances from exterior dependent nodes to the boundary. Therefore, the reconstructed
solution can account for the smooth movement of the immersed boundary.
Several numerical experiments have been conducted for two- and three-dimensional
moving-boundary flows. It is shown that the hybrid reconstruction approach can work
well in the finite-element context and effectively reduce the numerical oscillations with
little additional computational cost, and the spatial accuracy of the original local DFD
method can also be preserved. 相似文献
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求解多维欧拉方程的二阶非结构网格混合旋转Riemann求解器 总被引:2,自引:0,他引:2
将基于旋转近似Riemann求解器的二阶精度迎风型有限体积方法推广到非结构网格,采用基于网格中心的有限体积法,梯度的计算采用基于节点的方法引入更多的控制体模板,限制器的构造采用与非结构化网格相适应的形式.在求解Riemann问题时,沿具有一定物理意义的两个迎风方向,即控制体界面两侧速度差矢量方向及与之正交的方向.能够完全消除基于Riemann求解器的通量差分裂格式存在的激波不稳定或"红斑"现象.为减小计算量,采用HLL和Roe FDS混合旋转格式. 相似文献
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This paper presents efficient second-order kinetic schemes on unstructured meshes for both compressible unsteady and incompressible steady flows. For compressible unsteady flows, a time-dependent gas distribution function with a discontinuous particle velocity space at a cell interface is constructed and used for the evaluations of both numerical fluxes and conservative flow variables. As a result, a compact scheme on the unstructured meshes is developed. For incompressible steady flows, a continuous second-order gas-kinetic BGK type scheme is presented, for which the time-dependent gas distribution function with a continuous particle velocity is used on unstructured meshes. The efficiency of the schemes lies in the fact that the slopes of the flow variables inside each cell can be constructed using values of the flow variables within that cell only without involving neighboring cells. Therefore, even with the stencil of a first-order scheme, a high resolution method is constructed. Numerical examples are presented which are compared with the benchmark solutions and the experimental measurements. 相似文献