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1.
本文提出了一种基于自适应非结构化网格的VOF算法,根据相界面网格的相函数值对相界面网格进行自适应细化与合并,通过基于非结构化网格的界面构造方法构造相界面,在适量增加网格单元数量的情况下提高了计算的精度。该方法随着时间及相界面的变化无需重新整体生成网格,算法效率较高。经典算例的验证结果表明,本文自适应网格方法计算得到的结...  相似文献   

2.
采用非结构化网格有限容积法求解了不可压N-S方程组,对流项采用GAMMA格式,扩散项采用二阶中心差分格式建立离散方程,用SOAR算法处理压力与速度的耦合关系,得到了一种求解不可压N-S方程的非结构网格耦合求解器。通过方腔顶盖驱动流、后台阶绕流以及方腔自然对流等几个典型的算例,考察了求解器的计算精度及收敛特性,并与SIMPLE算法进行了比较,结果表明该求解器是有效可行的。  相似文献   

3.
网格单元形状对数值计算的影响   总被引:7,自引:0,他引:7  
实现了二维非结构化网格上的N-S方程的离散,编制了非结构化同位网格上的SIMPLE程序,针对CFD/NHT 中几个有基准解的问题进行了试算考核。结果表明,在步长基本相同的情况下,四边形网格的收敛速度和解的精度都优于 三角形网格,尤其是收敛速度更明显;使用考虑边界贴体特性的边界层网格,解的精度优于均匀网格。  相似文献   

4.
利用非结构化网格上的有限体积法对三维湍流进行了数值研究,提出了不用求解单元顶点处变量值的二阶混合差分格式,既避免了复杂耗时的单元顶点处变量值的计算,又避免了普通差分格式在非结构化网格上易于引起网格界面方向相关性问题。最后利用非结构化网格计算程序,数值求解了一台离心风机内叶轮及无叶扩压器通道内三维相对定常湍流,计算结果与实验值的比较表明速度的计算值与实验值吻合较好。  相似文献   

5.
为了增加涡旋压缩机啮合间隙处的动网格数量。本文根据涡旋压缩机的流体区域变化规律,提出一种结构化动网格的生成方法,实现了啮合间隙处的网格加密。进而得到一种基于结构化动网格的涡旋压缩机非定常流动的数值模拟方法;得到了任意时刻流体区域内的流场分布。与现有的非结构化动网格进行比较,结构化动网格解决了非结构化动网格在啮合间隙处易产生负体积的问题,能够在啮合间隙处生成足够的网格数量,提高了计算精度;且具有网格质量高、网格数量和疏密易控制等优点,更适合于涡旋压缩机工作过程的数值模拟计算。  相似文献   

6.
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   

7.
粘性不可压流体流动问题用直角坐标网格的贴体解法   总被引:1,自引:0,他引:1  
汪建兵  康宁 《计算物理》2004,21(4):290-298
研究一种新的全贴体的求解粘性不可压流体流动问题的非结构化直角坐标网格方法.该方法在于利用直角坐标网格但通过在边界附近保留不规则控制体,使得算法是完全贴体的.这有别于目前流行的各种非结构化直角坐标网格方法.通过对两个典型流动问题的计算对该数值方法进行验证.对比结果表明,本方法计算的结果与精确解和STAR—CD的结果在一定Re数和网格数时是很接近的,可以满足一定的精度要求,说明该数值计算方法是可行的.还对二维钝头体周围的流场进行了计算,计算的流场与STAR-CD的结果相当吻和,说明该算法还可计算较复杂的流动现象.  相似文献   

8.
本文针对单元中心非结构网格有限体积算法,通过构造上游虚节点和局部一维坐标,将结构化网格中常用的规正变量(NVSF)和总变差消失通量限制器(TVD FL)两种形式的传统高精度格式移植到非结构网格中。为了提高虚节点的插值精度,使用最小二乘法计算单元中心的变量梯度。经典算例考核并与商业软件FLUENT结果的比较表明,本文对非结构网格的高精度格式移植成功有效。  相似文献   

9.
非结构网格的生成及新型数据类型的应用   总被引:3,自引:0,他引:3  
本文基于 Delaunay三角化方法及局部重组的阵面推进法,给出了任意形状平面区域的非结构化网格剖分方法。文中对加点方法及数据结构和存取模式进行了改进,同时应用链表结构、动态数组和派生类型的数据变量,对算法进行优化,节省了计算内存,提高了网格的生成效率。本文研究为特殊计算区域的三维非结构化网格的生成提供了基本方法。  相似文献   

10.
提出了数值求解三维变系数对流扩散方程非等距网格上的四阶精度19点紧致差分格式,为了提高求解效率,采用多重网格方法求解高精度格式所形成的大型代数方程组。数值实验结果表明本文方法对于不同的网格雷诺数问题,在精确性、稳定性和减少计算工作量方面均明显优于7点中心差分格式。  相似文献   

11.
讨论非结构网格上温度扩散方程的能流计算方法.应用有限点方法(Finite Point Method,简称FPM)导出基于有限点两点公式和三点公式的能流计算公式,该公式适用于任意多边形及非匹配网格等非结构网格;给出网格角点温度新的计算公式.数值试验表明:基于两点公式的离散解和基于三点公式的离散解均具有平方阶的收敛速度;基于三点公式的离散解的精度总优于基于两点公式的离散解.  相似文献   

12.
Within realistic combustion devices, physical quantities may change by an order of magnitude over an extremely thin flamefront, while remaining nearly unchanged throughout large areas nearby. Such behaviour dictates the use of adaptive numerical methods. The recently developed local rectangular refinement (LRR) solution-adaptive gridding method produces robust unstructured rectangular grids, utilizes novel multiple-scale finite-difference discretizations, and incorporates a damped modified Newton's method for simultaneously solving systems of governing elliptic PDEs. Here, the LRR method is applied to two axisymmetric laminar flames: a premixed Bunsen flame with one-step chemistry and a diffusion flame employing various complex chemical mechanisms. The Bunsen flame's position is highly dependent upon grid spacing, especially on coarse grids; it stabilizes only with adequate refinement. The diffusion flame results show excellent agreement with experimental data for flame structure, temperature and major species. For both flames, the LRR results on intermediate grids are comparable to those obtained on equivalently refined conventional grids. Solution accuracy on the final LRR grids could not be achieved using conventional grids because the latter exceeded the available computer memory. In general, the LRR method required about half the grid points, half the memory and half the computation time of the solution process on conventional grids.  相似文献   

13.
在数值模拟中, 非结构网格的优势是可以采用相同的数值格式统一处理任意复杂的计算区域, 但在网格生成过程中难度大, 并且不容易控制网格质量。树结构网格可以认为是介于结构网格和非结构网格之间的一种网格, 目前已经有相对成熟的方法快速在复杂区域内生成二维四叉树网格和三维八叉树网格。在实际应用中, 数值方法往往需要在连接协调的非结构网格上做离散, 树结构网格中不同尺寸的网格之间连接不是协调的, 在应用上会受到很多限制。文章实现了树结构网格到非结构混合网格的转换, 这种转换在二维情况下就是将四叉树网格转换为非结构三角形和四边形的混合网格, 三维情况下则将八叉树网格转换为非结构混合网格。这一转换过程的难点在于需要考虑数千种不同的八叉树单元, 并给出能实现连接协调的非结构混合网格划分。可以出现的网格单元包括六面体、三棱柱、金字塔和四面体这4种不同情况。通过特别的分类, 实现了程序的自动生成, 这种程序自动生成技术一方面可以避免人工编写大量程序时的失误, 另一方面也使得对数以千计的不同情况的处理成为可能。通过对几个简单网格的测试, 对网格数据转换方法做了初步的验证。   相似文献   

14.
张荣培  蔚喜军  崔霞  冯涛 《计算物理》2012,29(5):647-653
提出一种求解二维非平衡辐射扩散方程的数值方法.空间离散上采用加权间断Galerkin有限元方法,其中数值流量的构造采用一种新的加权平均;时间离散上采用隐-显积分因子方法,将扩散系数线性化,然后用积分因子方法求解间断Galerkin方法离散后的非线性常微分方程组.数值试验中在非结构网格上求解了多介质的辐射扩散方程.结果表明:对于强非线性和强耦合的非线性扩散方程组,该方法是一种非常有效的数值算法.  相似文献   

15.
We develop a piecewise linear (PWL) Galerkin finite element spatial discretization for the multi-dimensional radiation diffusion equation. It uses recently introduced piecewise linear weight and basis functions in the finite element approximation and it can be applied on arbitrary polygonal (2D) or polyhedral (3D) grids. We first demonstrate some analytical properties of the PWL method and perform a simple mode analysis to compare the PWL method with Palmer’s vertex-centered finite-volume method and with a bilinear continuous finite element method. We then show that this new PWL method gives solutions comparable to those from Palmer’s. However, since the PWL method produces a symmetric positive-definite coefficient matrix, it should be substantially more computationally efficient than Palmer’s method, which produces an asymmetric matrix. We conclude that the Galerkin PWL method is an attractive option for solving diffusion equations on unstructured grids.  相似文献   

16.
非结构四边形网格下的一类保对称有限体元格式   总被引:3,自引:2,他引:1  
针对定常扩散问题,在非结构四边形网格下,通过选取特殊的控制体和有限体元空间,建立两种保对称有限体元格式,在拟一致网格剖分下,当扩散系数光滑时,证明有限体元解函数在L2和H1范数下均具有饱和误差阶.数值实验验证理论结果的正确性,同时表明新格式对扭曲大变形四边形网格、间断系数问题具有较强的适应性.在正交网格下,第二种格式对流(flux)函数在单元中心点的值还具有超逼近性.  相似文献   

17.
非结构混合网格上的NS方程求解方法   总被引:1,自引:0,他引:1  
王刚  叶正寅 《计算物理》2004,21(2):161-165
提出了一套较为通用的,完全自动化的非结构混合网格生成方法.在物面粘性作用区,采用一种改进的推进层方法生成三棱柱形和金字塔形网格;在其他流动区域采用阵面推进方法生成四面体网格.采用一种改进精度的格心有限体积法对三维NS方程进行了求解,在加速收敛措施方面,提出了一种新的当地时间步长取定方法来减小质量较差的网格单元对流场计算稳定性和收敛速度的不利影响.以M6机翼和DLR-F4翼身组合体外形的粘性流场作为数值算例,验证了上述网格生成和流场求解方法的正确性和实用性.  相似文献   

18.
The present work details the Elastoplast (this name is a translation from the French “sparadrap”, a concept first applied by Yves Morchoisne for Spectral methods [1]) Discontinuous Galerkin (EDG) method to solve the compressible Navier–Stokes equations. This method was first presented in 2009 at the ICOSAHOM congress with some Cartesian grid applications. We focus here on unstructured grid applications for which the EDG method seems very attractive. As in the Recovery method presented by van Leer and Nomura in 2005 for diffusion, jumps across element boundaries are locally eliminated by recovering the solution on an overlapping cell. In the case of Recovery, this cell is the union of the two neighboring cells and the Galerkin basis is twice as large as the basis used for one element. In our proposed method the solution is rebuilt through an L2 projection of the discontinuous interface solution on a small rectangular overlapping interface element, named Elastoplast, with an orthogonal basis of the same order as the one in the neighboring cells. Comparisons on 1D and 2D scalar diffusion problems in terms of accuracy and stability with other viscous DG schemes are first given. Then, 2D results on acoustic problems, vortex problems and boundary layer problems both on Cartesian or unstructured triangular grids illustrate stability, precision and versatility of this method.  相似文献   

19.
The paper explains a method by which discretizations of the continuity and momentum equations can be designed, such that they can be combined with an equation of state into a discrete energy equation. The resulting ‘MaMEC’ discretizations conserve mass, momentum as well as energy, although no explicit conservation law for the total energy is present. Essential ingredients are (i) discrete convection that leaves the discrete energy invariant, and (ii) discrete consistency between the thermodynamic terms. Of particular relevance is the way in which finite volume fluxes are related to nodal values. The method is an extension of existing methods based on skew-symmetry of discrete operators, because it allows arbitrary equations of state and a larger class of grids than earlier methods.The method is first illustrated with a one-dimensional example on a highly stretched staggered grid, in which the MaMEC method calculates qualitatively correct results and a non-skew-symmetric finite volume method becomes unstable. A further example is a two-dimensional shallow water calculation on a rectilinear grid as well as on an unstructured grid. The conservation of mass, momentum and energy is checked, and losses are found negligible up to machine accuracy.  相似文献   

20.
During the past two decades, the lattice Boltzmann (LB) method has been introduced as a class of computational fluid dynamic methods for fluid flow simulations. In this method, instead of solving the Navier Stocks equation, the Boltzmann equation is solved to simulate the flow of a fluid. This method was originally developed based on uniform grids. However, in order to model complex geometries such as porous media, it can be very slow in comparison with other techniques such as finite differences and finite elements. To eliminate this limitation, a number of studies have aimed to formulate the lattice Boltzmann on the unstructured grids. This paper deals with simulating fluid flow through a synthetic porous medium using the LB method and on the quadtree grid structure. To this end, the LB method was used on nonuniform grids coupled with a technique for image reconstruction which resulted in the quadtree grids for simulation of fluid flow through porous media. Accuracy and efficiency of this algorithm is compared against the conventional LB method based on uniform grids. While the decrease in computational time in the proposed LB method on nonuniform grids is found to be significant regarding the size of the initial and reconstructed images, the same level of accuracy is obtained when compared with the conventional LB method on uniform grids.  相似文献   

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