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Parallel simulation of incompressible free-surface flows.

机译:不可压缩自由表面流的并行模拟。

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摘要

A large number of computational problems and physical phenomena in areas such as fluid mechanics involve the motion of interfaces. Simulation of this type of problems is challenging. In this dissertation, an Arbitrary Lagrangian Eulerian (ALE) formulation is rigorously derived and a reduced form of ALE is implemented with various surface tracking techniques to simulate capillary jet breakup on a superposition-based parallel platform. The ALE formulation starts with an integral approach on moving control volumes and is converted into a format consistent with method-of-lines discretization. The weighted ALE is also formulated. Contradictions in existing differential approach of ALE formulation are pointed out and the paradoxical issue is clarified. The reduced ALE is used for formulation of incompressible Navier-Stokes flows on moving meshes. An indirect boundary tracking of flux method, decoupled non-Lagrangian direct boundary tracking (DBT), iterative non-Lagrangian DBT, and Lagrangian DBT are implemented for the highly sensitive capillary jet breakup. Excellent numerical results are obtained, which vindicates the success of the overall numerical method. The simulation is based on a superposition-based non-numeric parallelization, which takes a different approach from conventional domain decomposition. Element-by-element construction, superposition-based partition, and condensed random data structure are used for the data structure aspect of the parallelization. From the algorithm aspect of the parallelization, it maintains the same flow of data, control of process, and global structure as the serial counterpart. As a result, the parallelization features simplicity and portability in implementation yet achieves moderate performance. A three-dimensional semi-discontinuous finite element method serves as the domain solver for all calculations, and is adequately verified with fixed-geometry benchmark problems. Various time schemes, including a proposed linear implicit scheme with excellent performance, are implemented generically. The indefinite system as a result of incompressible flows is tackled with a proposed discrete operator splitting technique, which breaks a large ill-natured discrete equation system into well-natured subsystems through source-term iterations.
机译:诸如流体力学之类的领域中的大量计算问题和物理现象涉及界面的运动。模拟这类问题具有挑战性。本文严格推导了任意的拉格朗日欧拉公式,并采用多种表面跟踪技术实现了ALE的简化形式,以模拟基于叠加的并行平台上的毛细喷射破裂。 ALE公式从移动控制量的整体方法开始,然后转换为与线法离散化一致的格式。还制定了加权ALE。指出了现有的ALE制定方法的矛盾之处,并阐明了矛盾的问题。减少的ALE用于在移动的网格上公式化不可压缩的Navier-Stokes流。通量方法的间接边界跟踪,去耦非拉格朗日直接边界跟踪(DBT),迭代非拉格朗日DBT和拉格朗日DBT用于实现高灵敏度的毛细管喷射破裂。获得了出色的数值结果,证明了整体数值方法的成功。该模拟基于基于叠加的非数字并行化,采用与常规域分解不同的方法。并行化的数据结构方面使用逐元素构造,基于叠加的分区和压缩的随机数据结构。从并行化的算法方面来看,它与串行对应项保持相同的数据流,过程控制和全局结构。结果,并行化具有实现过程中的简单性和可移植性,但仍具有中等性能。三维半不连续有限元方法用作所有计算的域求解器,并已通过固定几何基准问题进行了充分验证。一般地实现各种时间方案,包括所提出的具有优异性能的线性隐式方案。通过提出的离散算子拆分技术解决了由于不可压缩流导致的不确定系统,该技术通过源项迭代将一个大型,性质不佳的离散方程组分解为性质良好的子系统。

著录项

  • 作者

    Zhang, Keqin.;

  • 作者单位

    University of Illinois at Chicago.;

  • 授予单位 University of Illinois at Chicago.;
  • 学科 Engineering Mechanical.
  • 学位 Ph.D.
  • 年度 2009
  • 页码 132 p.
  • 总页数 132
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类 遥感技术;
  • 关键词

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