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Practical implementation of robust preconditioners for optimized multistage flow solvers.

机译:坚固的预处理器的实际实现,用于优化的多级流量求解器。

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摘要

Explicit multistage multigrid methods have carved their niche in the solution of complex inviscid and viscous flows. Because of their scalable parallel implementations, they have been a popular choice for the solution of large-scale, complex configuration problems. The convergence rate of these methods deteriorates when they face problems such as numerical stiffness or directional decoupling that result from propagative disparity, cell stretching, and flow alignment. Moreover, in the limit of low Mach numbers, most compressible flow solvers become ill-conditioned in addition to losing accuracy. It is possible to improve existing codes that typically use local time-stepping by using squared preconditioning schemes that combine Block-Jacobi preconditioning with low-Mach preconditioning. A robust and practical implementation of a squared preconditioner is possible for both Euler and Navier-Stokes equations when using an analytical form in entropy variables and their corresponding transformation matrices. Particular attention must be given to entropy fix and limiting techniques. Results of this squared preconditioned approach are presented for both two- and three-dimensional test cases. For these test cases the preconditioning produces convergence acceleration for all Mach numbers while always maintaining the accuracy of the solution. Additional convergence acceleration can be obtained via the optimization of various input parameters such as multistage coefficients, artificial dissipation coefficients and the CFL numbers.
机译:显式的多级多网格方法已经在复杂的无粘性和粘性流解决方案中占据了优势。由于它们具有可伸缩的并行实现,因此它们已成为解决大规模复杂配置问题的流行选择。当这些方法面临由于传播差异,单元拉伸和流动对齐而导致的数值刚度或方向性解耦之类的问题时,其收敛速度会降低。而且,在低马赫数的极限下,大多数可压缩的流量求解器除了失去准确性外,还会变得病态。通过使用结合了Block-Jacobi预处理和Low-Mach预处理的平方预处理方案,可以改善通常使用本地时间步长的现有代码。当在熵变量及其对应的变换矩阵中使用解析形式时,对于Euler和Navier-Stokes方程,都可以对平方的预处理器进行鲁棒且实用的实现。必须特别注意熵固定和限制技术。针对二维和三维测试用例均提供了这种平方的预处理方法的结果。对于这些测试用例,预处理可为所有马赫数产生收敛加速,同时始终保持求解的准确性。通过优化各种输入参数(例如多级系数,人工耗散系数和CFL数),可以获得额外的收敛加速。

著录项

  • 作者

    Hosseini, Kaveh.;

  • 作者单位

    Stanford University.;

  • 授予单位 Stanford University.;
  • 学科 Engineering Aerospace.
  • 学位 Ph.D.
  • 年度 2005
  • 页码 140 p.
  • 总页数 140
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类 航空、航天技术的研究与探索;
  • 关键词

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