首页> 外文会议>15th AIAA/CEAS aeroacoustics conference 2009 (30th AIAA aeroacoustics conference) >Nonuniform Time-step Runge-Kutta Discontinuous Galerkin Method for Computational Aeroacoustics
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Nonuniform Time-step Runge-Kutta Discontinuous Galerkin Method for Computational Aeroacoustics

机译:计算航空声学的非均匀时间步长Runge-Kutta间断Galerkin方法

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In computational aeroacoustics (CAA) simulations, discontinuous Galerkin space discretization (DG) in conjunction with Runge-Kutta time integration (RK), which is so called Runge-Kutta discontinuous Galerkin method (RKDG), has been an attractive alternative to the finite difference based high-order numerical approaches. However, when it comes to complex physical problems, especially the ones involving irregular geometries, an expensive computational cost are usually required for time-accurate solution, because the time step size of an explicit RK scheme is limited by the smallest grid size in the computational domain. For computational efficiency, high-order RK method with nonuniform time step sizes on nonuniform meshes is developed in this paper. On the elements neighboring the interfaces of grids with different time step sizes, the values at intermediate stages of RK time integration are coupled suitably to realize the stable communication of solutions at those interfaces with minimal dissipation and dispersion errors. A linear coupling procedure is described based upon the general form of a p-stage RK scheme, and also extended to the high-order RK schemes frequently used in simulation of fluid flow and acoustics, including the third order TVD scheme, and low-storage low dissipation and low dispersion schemes. In addition, an eigenvalue analysis of nonuniform time-step RK integration combined with DG method on a nonuniform grid is carried out for the stability property. For verification, numerical experiments on one-dimensional and two-dimensional linear problems are conducted to illustrate the stability and accuracy of proposed nonuniform time-step RKDG scheme. Application to a one-dimensional nonlinear problem is also investigated.
机译:在计算空气声(CAA)模拟中,不连续的Galerkin空间离散化(DG)与Runge-Kutta时间集成(RK)相结合,即所谓的Runge-Kutta不连续的Galerkin方法(RKDG),这是有限差异的有吸引力的替代方案基于高阶数值方法。然而,当涉及复杂的身体问题时,特别是涉及不规则几何形状的物理问题,通常需要昂贵的计算成本,因为时间准确的解决方案,因为显式RK方案的时间步长受到计算中最小的网格尺寸的限制领域。为了计算效率,本文开发了非均匀网格上具有非均匀时间步长的高阶RK方法。在具有不同时间步长的网格接口的元素上,RK时间集成的中间阶段的值适当地耦合,以实现具有最小耗散和色散误差的这些接口的稳定性通信。基于P-阶段RK方案的一般形式描述了线性耦合过程,并且还扩展到经常用于流体流动和声学模拟的高阶RK方案,包括第三阶TVD方案和低存储器低耗散和低分散方案。此外,对稳定性的性能进行了与非均匀网格中的DG方法结合的非均匀时间步骤RK积分的特征值分析。为了验证,进行了一维和二维线性问题的数值实验,以说明所提出的非均匀时间步骤RKDG方案的稳定性和准确性。还研究了在一维非线性问题的应用。

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