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Efficient Runge-Kutta Discontinuous Galerkin Methods Applied to Aeroacoustics

机译:应用于航空声学的高效Runge-Kutta间断Galerkin方法

摘要

The simulation of aeroacoustic problems sets demanding requirements on numerical methods, particularly in terms of accuracy. Runge-Kutta Discontinuous Galerkin (RKDG) schemes are increasingly popular for such applications, because they converge at an arbitrarily high order rate, they can deal with complex geometries, and they are amenable to parallel computing. However, they are still considered to be computationally costly. The work presented in this thesis aims at improving the computational efficiency of RKDG methods for linear aeroacoustic applications.The first part of the work is dedicated to the study of the stability and accuracy properties that affect the performance of RKDG methods applied to hyperbolic problems. An analysis technique inspired by the classical von Neumann method is used to determine the stability restrictions of the schemes, as well as their accuracy properties in terms of dissipation and dispersion. It is first used to investigate the influence of the element shape on CFL conditions with triangular grids, in order to improve the determination of the maximum allowable time step in practical simulations. Alternative methods to the CFL conditions are also devised for this purpose. Moreover, Runge-Kutta schemes specifically designed to maximize the computational efficiency of RKDG methods for wave propagation problems are derived.The second part of the work deals with the application of RKDG methods to linear aeroacoustics. RKDG formulations for the linearized Euler and Navier-Stokes equations are introduced, along with validation cases. Then, higher-order treatments of curved wall boundaries, needed to fully benefit from the efficiency of high-order RKDG methods in aeroacoustic propagation problems, are studied. Finally, the methods developed in this work are used in a hybrid approach to characterize the acoustic behaviour of orifices in plates under grazing flow. The results show a clear qualitative improvement over the existing analytical approaches.
机译:航空声学问题的模拟对数值方法提出了苛刻的要求,尤其是在精度方面。 Runge-Kutta间断Galerkin(RKDG)方案在此类应用中越来越受欢迎,因为它们以任意高的阶数收敛,可以处理复杂的几何形状,并且适合并行计算。然而,它们仍然被认为在计算上是昂贵的。本文的工作旨在提高用于线性航空声学应用的RKDG方法的计算效率。研究的第一部分致力于研究影响RKDG方法应用于双曲问题的性能的稳定性和准确性。采用经典冯·诺依曼(von Neumann)方法启发的分析技术来确定方案的稳定性限制,以及它们在耗散和色散方面的准确性。它首先用于研究带有三角形网格的元素形状对CFL条件的影响,以便在实际仿真中改进对最大允许时间步长的确定。为此目的,还设计了CFL条件的替代方法。此外,推导了专门设计用于最大化RKDG方法用于波传播问题的计算效率的Runge-Kutta方案。第二部分工作涉及RKDG方法在线性航空声学中的应用。介绍了线性Euler和Navier-Stokes方程的RKDG公式以及验证案例。然后,研究了充分利用高阶RKDG方法在航空声传播问题中的效率所需要的弯曲壁边界的高阶处理。最后,在这项工作中开发的方法以混合方式使用,以表征掠流下板中孔口的声学特性。结果表明,与现有的分析方法相比,其质量有了明显的提高。

著录项

  • 作者

    Toulorge Thomas;

  • 作者单位
  • 年度 2012
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  • 原文格式 PDF
  • 正文语种 nl
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