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Modifying an Unstructured Roe Solver for Large Eddy Simulation

机译:修改用于大涡模拟的非结构化鱼卵求解器

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With the ever increasing availability of computing power, attention is being turned to large eddy simulation as a design tool at the component level. To maintain integration with pre-existing design processes based on solving the Reynolds Averaged Navier-Stokes equations, legacy RANS codes are being pressed into service with minimal adaptation to perform large eddy simulations. Often, these legacy RANS solvers are based around the approximate Riemann solver of Roe. It is shown here that the Roe scheme is not ideally suited to large eddy simulations, and may require excessive user care to extract worthwhile information — a process not always possible within design timeframes. A different discretisation scheme, which is shown to conserve kinetic energy, but which also shares some of the favourable structural behaviour of Roe's is implemented, and is then tested on a range of geometries, both canonical and industrial. One of the advantages of this approach is its ability to eliminate the smoothing terms which have a strong deleterious affect on the LES performance of Roe. This allows exph'cit subgrid models to be sensibly applied. The new scheme, with explicit turbulence modelling, is found to outperform the Roe scheme for LES in all of the test cases.
机译:随着计算能力的日益提高,人们越来越关注大型涡流仿真作为组件级设计工具。为了保持基于解决雷诺平均Navier-Stokes方程的现有设计流程的集成,将传统的RANS代码以最小的适应性投入使用,以执行大型涡流仿真。通常,这些传统的RANS求解器基于Roe的近似Riemann求解器。这里表明,Roe方案并不理想地适合于大型涡流仿真,并且可能需要过多的用户维护才能提取有价值的信息-在设计时限内并不总是可能进行此过程。实现了一种不同的离散化方案,该方案可以节省动能,但也可以共享Roe的一些良好的结构行为,然后在规范化和工业化的一系列几何结构上进行测试。这种方法的优点之一是它能够消除对Roe的LES性能具有严重有害影响的平滑项。这使得可以合理地应用exph'cit子网格模型。在所有测试案例中,发现了具有显式湍流建模的新方案,其性能优于LES的Roe方案。

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