首页> 外文会议>AIAA computational fluid dynamics conference;AIAA aviation forum >Subgrid-scale modeling and implicit numerical dissipation in DG-based Large-Eddy Simulation
【24h】

Subgrid-scale modeling and implicit numerical dissipation in DG-based Large-Eddy Simulation

机译:基于DG的大涡模拟中的亚网格尺度建模与隐性数值耗散。

获取原文

摘要

Over the past few years, high-order discontinuous Galerkin (DG) methods for Large-Eddy Simulation (LES) have emerged as a promising approach to solve complex turbulent flows. However, despite the significant research investment, the relation between the discretization scheme, the subgrid-scale (SGS) model and the resulting LES solver remains unclear. This paper aims to shed some light on this matter. To that end, we investigate the role of the Riemann solver, the SGS model, the time resolution, and the accuracy order in the ability to predict a variety of flow regimes, including transition to turbulence, wall-free turbulence, wall-bounded turbulence, and turbulence decay. The transitional flow over the Eppler 387 wing, the Taylor-Green vortex problem and the turbulent channel flow are considered to this end. The focus is placed on post-processing the LES results and providing with a rationale for the performance of the various approaches.
机译:在过去的几年中,用于大涡模拟(LES)的高阶不连续Galerkin(DG)方法已经成为解决复杂湍流的一种有前途的方法。然而,尽管投入了大量的研究资金,但离散化方案,子网格规模(SGS)模型与生成的LES解算器之间的关系仍然不清楚。本文旨在阐明这一问题。为此,我们研究了黎曼求解器的作用,SGS模型,时间分辨率和精度顺序,以预测各种流动状态,包括过渡到湍流,无壁湍流,有壁湍流和湍流衰减。为此,考虑了埃普勒387机翼上的过渡流,泰勒-格林涡旋问题和湍流通道流。重点放在对LES结果的后处理上,并为各种方法的性能提供理论依据。

著录项

相似文献

  • 外文文献
  • 中文文献
  • 专利
获取原文

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号