三角网格细分技术在三维地质模型中的应用

针对目前三维地质建模过程中建模速度慢,地质模型效果差的现状,全面总结了常用的三角网格细分方案,利用地质专家筛选出的少量有效数据,通过气角网格细分技术进行三维地质模型构造,以加快其生成速度和提高地质模型的质量。     

室内人体移动过程对热舒适的影响研究

使用计算流体力学(CFD)技术,结合动网格技术和刚体运动学理论,对室内人体移动进行了动态模拟,得到了人体移动过程中不同时刻室内流场分布.分析了移动过程中的平均温度、平均速度、温度和速度不均匀性指标,并预测了有效吹风温度(TEDT)、空气分布特性指标(ADPI)和吹风感的不满意率指标(PD),比较了不同人体移动速度对以上指标的影响.模拟结果表明,人体移动对室内气流分布和热舒适有短期影响,能提高室内风速的扰动,造成吹风感.     

一类雨量预报准确性评价方法

给出了一种利用网格点的预报雨量来模拟区域内任一点预报雨量的方法,建立了预报雨量函数,进而得出预报雨量与实测雨量的整体偏方差的数学模型;利用QPF方法建立出准确率、预报效率、空报率、漏报率等评价预报方法优劣指标的数学模型,并对两种预报方法得出的数据进行了计算,得出上述模型中的数值如下:方案方法总体偏方差预报准确率漏报率空报率预报效率方法1 0.99987×10679.431%11.463%25.621%62.256%方法2 1.00518×10657.509%26.976%31.705%58.936%比较这些指标,可得第一种预报结果较好.     

基于瑞利分布的计量型序贯网图检验

针对瞄准发射系统中着落点位置通常服从瑞利分布的事实,研究了计量型检验问题,建立了基于瑞利分布的序贯网图检验.采用搜索和迭代的计算机程序,可以得到计量型序贯网图检验方案.通过实例将序贯网图与计量型定数检验和计量型序贯概率比检验进行比较.结果显示,计量型序贯网图检验在减小最大样本量方面有更好的效果,更适用于高成本的抽样检验.     

双大Reynolds数问题的混合方法

讨论双大Reynolds数问题,首先将解析解分解为光滑部分和奇性部分,对这两部分都做了上界估计;然后将解析解进行2阶渐近展开;最后提出混合算法．混合算法的主要思想是引入过渡点将区域分为粗网格区域和细网格区域,在这些网格区域采用等步长．在细网格区域采用有限元法,在粗网格区域采用迎风差分格式．混合算法结合了渐近解、数值解和BVT法的优势,是一个实用、有效的算法。     

A control volume finite element method for three-dimensional three-phase flows

A novel control volume finite element method with adaptive anisotropic unstructured meshes is presented for three-dimensional three-phase flows with interfacial tension. The numerical framework consists of a mixed control volume and finite element formulation with a new P₁DG-P₂ elements (linear discontinuous velocity between elements and quadratic continuous pressure between elements). A “volume of fluid” type method is used for the interface capturing, which is based on compressive control volume advection and second-order finite element methods. A force-balanced continuum surface force model is employed for the interfacial tension on unstructured meshes. The interfacial tension coefficient decomposition method is also used to deal with interfacial tension pairings between different phases. Numerical examples of benchmark tests and the dynamics of three-dimensional three-phase rising bubble, and droplet impact are presented. The results are compared with the analytical solutions and previously published experimental data, demonstrating the capability of the present method.     

Evolution of vortices in the wake of an ARJ21 airplane: Application of the lift-drag model

Wake separation is crucial to aircraft landing safety and is an important factor in airport operational efficiency. The near-ground evolution characteristics of wake vortices form the foundation of the wake separation system design. In this study, we analysed the near-ground evolution of vortices in the wake of a domestic aircraft ARJ21 initialised by the lift-drag model using large eddy simulations based on an adaptive mesh. Evolution of wake vortices formed by the main wing, flap and horizontal tail was discussed in detail. The horizontal tail vortices are the weakest and dissipate rapidly, whereas the flap vortices are the strongest and induce the tip vortex to merge with them. The horizontal tail and flap of an ARJ21 do not significantly influence the circulation evolution, height change and movement trajectory of the wake vortices. The far-field evolution of wake vortices can therefore be analysed using the conventional wake vortex model.     

ANSYS网格划分技巧与网格信息提取技术

有限元软件ANSYS 在模型的网格划分方面功能非常强大.通过举例说明了如何用ANSYS 参数设计语言生成网格,并提供了相应的宏命令文件.随后,用Fortran 语言编写了将CDB 文本文件中的网格信息转换成自编程序可以识别的网格数据的Fortran 源程序.该程序适用于由SHELL93 单元所生成的网格.     

一类无结构三角网上抛物方程的有限差分区域分解算法

本文讨论了一类在无结构三角网上数值求解二维热传导方程的有限差分区域分解算法．在这个算法中,将通过引进两类不同类型的内界点,将求解区域分裂成若干子区域．一旦内界点处的值被计算出来,其余子区域上的计算可完全并行．本文得到了稳定性条件和最大模误差估计,它表明我们的格式有令人满意的稳定性和较高的收敛阶．     

THE GENERALIZED MAXIMUM ANGLE CONDITION FOR THE Q1 ISOPARAMETRIC ELEMENT

We consider the quadrilateral Q1 isoparametric element and establish an optimal error estimate in H^1 norm for the interpolation operator under a weaker mesh condition which admits anisotropic quadrilaterals and allows the quadrilateral to become a regular triangle in the sense of maximum angle condition [5, 11].