共查询到16条相似文献,搜索用时 62 毫秒
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有限元分析的精度和效率与网格划分的质量有直接关系.目前尚缺乏一种普适性的自动网格划分方法,尤其是对于具有多种几何特征的复杂模型,现有的六面体网格自动划分算法存在不同几何特征间的网格兼容性较差以及孔状特征周围网格质量不高的问题.对此本文提出一种基于映射法的六面体网格自动生成方法,在映射法的基本框架下,将物理空间中的复杂几何体映射为计算空间中的规则几何体,引入边界顶点分类,将复杂几何体边界进行简化,将子域约束进行连接,寻找贯穿边界,以使映射网格在约束特征间兼容;对圆弧特征进行等效转化,降低曲率过大对于网格过渡的影响.实例验证表明,本方法稳定可靠,生成的六面体网格质量较高,能够解决多特征复杂几何体六面体网格自动划分问题. 相似文献
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以映射法为基础并结合网格划分经验,提出了原理简单的六面体网格生成新办法.该方法根据物体轮廓选择初始网格,设定表面结点强制变形到目的曲面,经由有限元弹性计算确定内部节点的位置.在检查全体单元质量以后,调整畸形单元从而生成目的网格.通过为一个复杂的马头门模型构建全六面体网格,最后证明了本文所述方法的可行性. 相似文献
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平面区域四边形网格自动生成技术 总被引:5,自引:0,他引:5
本文分析和综述了四边形网格自动生成的各种算法,给出了三角形网格向四边形网格转换的局部算法,以及有FGT思想直接生成四边形和三角形网格算法。详细分析了此法之下生成网格的几何拓朴性质,最后给出实例验证了算法的有效性。 相似文献
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河道砂油藏的自适应非均匀网格粗化算法 总被引:6,自引:1,他引:5
以河道砂的观测深度为确定性数据,由贝叶斯理论通过随机楚模的方法楚立横截面为抛物线形状的河道砂油藏边界面,并将渗透率自适应网格技术应用于河道砂油藏的网格粗化算法中。在渗透率或孔隙度交化异常区域自动采用精细网格,用直接解法求解渗透率或孔隙度交化异常区域的压强分布,而在其他区域采用不均匀网格粗化方法计算,印在流体流速大的区域采用精细网格。用本文方法计算了河道砂油藏的压强分布,结果表明河道砂油藏的三维不均匀自适应网格粗化算法的解在渗透率或孔隙度异常区的压强分布规律更逼近采用精细网格的解,在其他区域压强分布规律非常逼近粗化算法的解,但计算的速度比采用精细网格提高了100多倍。 相似文献
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针对无网格Galerkin法在三维复杂几何形状的结构分析中存在的刚度矩阵的稀疏存储实现难、六面体背景网格适应性差等问题,本文采用逐节点对法组装刚度矩阵,利用CSR格式存储刚度矩阵,提出了一种基于四面体背景积分的改进的三维无网格Galerkin法。通过采用罚函数法施加对称约束和给定位移值约束,并推导出了施加这两种位移约束的统一格式。利用所提算法完成了三维悬臂梁的计算,所得结果与其理论解相吻合;完成了轴流式风机轮毂的结构分析,得到的位移与应力分布结果与其有限元解相吻合。这表明本文所提方法能满足工程应用中的计算要求,并适用于具有复杂形状的几何模型分析。 相似文献
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There are some approaches for all‐hexahedral mesh quality improvement by means of node‐movement while preserving the connectivity. Among these methods, the most easily implemented and well known one is the Laplacian smoothing method; however, for this method mesh quality improvement is not guaranteed in all cases, and this approach might cause inverted elements especially in concave regions. In this work, a method for the improvement of hexahedral mesh shape‐quality without causing inverted elements is proposed; which is based on optimization of an objective function calculated by means of the individual qualities of hexahedral elements in the mesh. The shape‐quality for each hexahedral element is defined via the condition number of the relevant element. The numerical optimization scheme is the particle swarm optimization method, which originated from observations related to the social behaviors of bird, insect, or fish colonies. The purpose of this paper is to discuss the applicability of this approach to mesh smoothing. Some examples are given in order to demonstrate the applicability. Copyright © 2008 John Wiley & Sons, Ltd. 相似文献
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In this paper we investigate local adaptive refinement of unstructured hexahedral meshes for computations of the flow around the DU91 wind turbine airfoil. This is a 25% thick airfoil, found at the mid‐span section of a wind turbine blade. Wind turbine applications typically involve unsteady flows due to changes in the angle of attack and to unsteady flow separation at high angles of attack. In order to obtain reasonably accurate results for all these conditions one should use a mesh which is refined in many regions, which is not computationally efficient. Our solution is to apply an automated mesh adaptation technique. In this paper we test an adaptive refinement strategy developed for unstructured hexahedral meshes for steady flow conditions. The automated mesh adaptation is based on local flow sensors for pressure, velocity, density or a combination of these flow variables. This way the mesh is refined only in those regions necessary for high accuracy, retaining computational efficiency. A validation study is performed for two cases: attached flow at an angle of 6° and separated flow at 12°. The results obtained using our adaptive mesh strategy are compared with experimental data and with results obtained with an equally sized non‐adapted mesh. From these computations it can be concluded that for a given computing time, adapted meshes result in solutions closer to the experimental data compared to non‐adapted meshes for attached flow. Finally, we show results for unsteady computations. Copyright © 2005 John Wiley & Sons, Ltd. 相似文献
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An Assessment of Detached-Eddy Simulations of Unsteady Crosswind Aerodynamics of Road Vehicles 总被引:2,自引:0,他引:2
In this paper, the availability of Detached-Eddy Simulations (DES) for simulating unsteady crosswind aerodynamics in industrial applications is explored and reported. The flow around a simple car geometry under headwind, steady crosswind and time-dependent wind gust respectively, is analysed for two different types of mesh using a commercial software, STAR-CD. The typical Reynolds number of the flow cases studied is 2.0 · 106 based on the vehicle length. The performances of polyhedral meshes together with a comparable hexahedral mesh are evaluated for capturing the time development of the flow structures during a gust. From the results presented, it can be concluded that the aerodynamic coefficients can be reliably calculated using both polyhedral and hexahedral meshes, although the fine turbulent structures in the wake are better captured with the hexahedral mesh. Using turbulence methods like DES in order to resolve the flow scales provides a significant insight for designing a ground vehicle and, due to the reasonable computational times involved, can hence be foreseen to be incorporated in a design process in a near future. 相似文献
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基于单元几何变形操作提出一种高效的非结构网格质量修匀方法。其基本过程是先对每个单元独立地进行拉伸-收缩操作以优化单元的形状,然后在整个网格中通过对各单元的节点位置进行加权平均来获得改善后的网格。为进一步提高修匀方法对网格质量的优化效果,并使得该方法具备一定的网格调整能力,结合动网格技术提出了对单元进行大范围和较大幅度移动的策略;在修匀过程中还通过适当算法调整单元形心位置和单元尺寸,进一步增强了修匀方法对网格局部进行疏密调节的能力。本文方法可适用于平面和三维非结构网格的质量改善及网格调整。若干算例表明了方法的有效性。 相似文献