The capability to incorporate moving geometric features within models for complex simulations is a common requirement in many fields. Fluid mechanics within aeronautical applications, for example, routinely feature rotating (e.g. turbines, wheels and fan blades) or sliding components (e.g. in compressor or turbine cascade simulations). With an increasing trend towards the high-fidelity modelling of these cases, in particular combined with the use of high-order discontinuous Galerkin methods, there is therefore a requirement to understand how different numerical treatments of the interfaces between the static mesh and the sliding/rotating part impact on overall solution quality. In this article, we compare two different approaches to handle this non-conformal interface. The first is the so-called mortar approach, where flux integrals along edges are split according to the positioning of the non-conformal grid. The second is a less-documented point-to-point interpolation method, where the interior and exterior quantities for flux evaluations are interpolated from elements lying on the opposing side of the interface. Although the mortar approach has significant advantages in terms of its numerical properties, in that it preserves the local conservation properties of DG methods, in the context of complex 3D meshes it poses notable implementation difficulties which the point-to-point method handles more readily. In this paper we examine the numerical properties of each method, focusing not only on observing convergence orders for smooth solutions, but also how each method performs in under-resolved simulations of linear and nonlinear hyperbolic problems, to inform the use of these methods in implicit large-eddy simulations.
翻译:将移动几何特征纳入复杂模拟模型中的能力是许多领域的共同要求。 航空应用中流力力力力学常态旋转(如涡轮机、轮轮和风扇刀片)或滑动部件(如压缩机或涡轮机级联模拟)或滑动部件(如压缩机或涡轮机级联模拟)等常规性旋转(如压缩机或涡轮机级联级机)或滑动部件(如压缩机或涡轮机级联动机或涡轮机级联级联)等,随着对这些案例采用高度不易碎建模型的趋势,特别是采用高阶不连续的Galerkin方法,因此需要了解静态网状网状网状网状网状网状网状和滑动/旋转部分对整体解决方案质量的影响之间如何不同的数字趋同。 在本文章中,我们比较两种不同的方法是迫击炮法系非优势的,在每一条形线状网状上,在每一条形线形线上也显示非优势,在每一条状线状线上显示其精确的伸缩方法的伸缩方法中,从而保持了这些稳定的内压方法的特性。