首页> 外文期刊>Journal of Computational Physics >Three-dimensional boundary conditions for direct and large-eddy simulation of compressible viscous flows
【24h】

Three-dimensional boundary conditions for direct and large-eddy simulation of compressible viscous flows

机译:可压缩粘性流直接和大涡模拟的三维边界条件

获取原文
获取原文并翻译 | 示例
获取外文期刊封面目录资料

摘要

Navier-Stokes characteristic boundary conditions (NSCBC) usually assume the flow to be normal to the boundary plane. In this paper, NSCBC is extended to account for convection and pressure gradients in boundary planes, resulting in a 3D-NSCBC approach. The introduction of these additional transverse terms requires a specific treatment for the computational domain's edges and corners, as well as a suited set of compatibility conditions for boundaries joining regions associated to different flow properties, as inlet, outlet or wall. A systematic strategy for dealing with edges and corners is derived and compatibility conditions for inlet/outlet and wall/outlet boundaries are proposed. Direct numerical simulation (DNS) tests are carried out on simplified flow configurations at first. 3D-NSCBC brings a drastic reduction of flow distortion and numerical reflection, even in regions of strong transverse convection; the accuracy and convergence rate toward target values of flow quantities is also improved. Then, 3D-NSCBC is used for large-eddy simulation (LES) of a free jet and an impinging round-jet. Edge and corner boundary treatment, combining multidirectional characteristics and compatibility conditions, yields stable and accurate solutions even with mixed boundaries characterized by bad posedness issues (e.g. inlet/outlet). LES confirms the effectiveness of the proposed boundary treatment in reproducing mean flow velocity and turbulent fluctuations up to the computational domain limits. (C) 2008 Elsevier Inc. All rights reserved.
机译:Navier-Stokes特征边界条件(NSCBC)通常假定流垂直于边界平面。本文将NSCBC扩展为考虑边界平面中的对流和压力梯度,从而产生了3D-NSCBC方法。这些其他横向术语的引入要求对计算域的边缘和角进行特殊处理,并为连接与不同流动特性相关的区域(如入口,出口或壁)的边界的边界设置合适的一组相容性条件。推导了一种处理边缘和拐角的系统策略,并提出了入口/出口和壁/出口边界的相容条件。首先,对简化的流量配置执行直接数值模拟(DNS)测试。 3D-NSCBC即使在强烈的横向对流区域中也可以大大减少流动畸变和数值反射;朝向流量目标值的精度和收敛速度也得到了提高。然后,将3D-NSCBC用于自由射流和撞击圆形射流的大涡模拟(LES)。边缘和拐角边界处理结合了多向特性和兼容性条件,即使在混合边界存在不良姿势问题(例如入口/出口)的情况下,也可以提供稳定,准确的解决方案。 LES证实了所提出的边界处理方法在再现平均流速和湍流波动直至计算域极限方面的有效性。 (C)2008 Elsevier Inc.保留所有权利。

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