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An Adaptive Finite Element Technique with Dynamic LES for Incompressible and Compressible Flows

机译:一种适用于不可压缩和可压缩流动动态LES的自适应有限元技术

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Large-eddy simulation (LES) is a technique intermediate between the direct simulation of turbulent flows and the solution of the Reynolds-averaged Navier-Stokes (RANS) equations. In LES the contribution of the large, energy-carrying structures to momentum and energy transfer is computed exactly, and only the effect of the smallest scales of turbulence is modeled. Small scales tend to be more homogeneous and universal, and less affected by the boundary conditions than the larger scales. LES models can be simpler and require fewer adjustments when applied to different flows than similar models for the RANS equations. Moreover, for fluid flow applications involving chemical reactions, which take place in the small scale structures of the turbulence, LES including species and particle transport naturally constitutes a more accurate model. Here we present our methods and results for an LES turbulence model that was developed for the KIVA combustion software, which is part of a larger effort to enhance combustion predictability and efficiencies within engines. In this study, the Vreman dynamic LES approach by Lau [2012] is implemented in a Predictor-Corrector Split (PCS) h-adaptive Finite Element Method (FEM) for modeling combustion. The PCS h-adaptive FEM model achieves 2nd and higher order spatial accuracy, with a minimal amount of computational effort (Carrington et al. [2013]). In our formulation, the Vreman dynamic LES model is able to solve compressible and incompressible fluid flow without any wall damping function or ad-hoc clipping to prevent an unstable (negative) eddy viscosity, unlike the Smagorinsky subgrid model (SM). Furthermore, it provides measurement of the actual error in the discretization, and can adjust spatial accuracy to minimize the error to some specified amount. By utilizing the dynamic model, the flow can be automatically classified as laminar or turbulent as it develops, improving the resolution of eddy viscosity. The goal is to use this dynamic LES PCS hp-adaptive FEM code, known as KIVA-hpFE, for reacting flows with complex geometries found in internal combustion engines. In the present paper, the dynamic Vreman LES approach is described for a simple geometry concerning the discretization schemes for the mass, momentum, energy and species transport equations and for SGS stress modeling. The problem configuration deals with unsteady turbulent flow problem over a backward facing step (BFS). Previous work by Carrington et al [2013] showed the ability of KIVAhpFE to accurately capture shocks and shock-wave/boundary layer interactions, and simulations were in good agreement with experimental data. In this study, the reattachment length and instantaneous flow results for the backward-facing step compare well with published simulations and experimental data.
机译:大涡模拟(LES)是一种技术中间的湍流流程和雷诺平均Navier-Stokes(RAN)方程的溶液的直接模拟。在LES中,恰好计算了大,能量携带结构与动量和能量传递的贡献,并且仅建模了最小湍流的效果。小鳞片往往是更均匀的和普遍的,并且受边界条件的影响越来越小。 LES模型可以更简单,并且在应用于不同流量的流量时需要更少的调整,而不是RAN方程的类似模型。此外,对于涉及化学反应的流体流动应用,其在湍流的小规模结构中发生,包括物种和颗粒传输的LES自然构成更准确的模型。在这里,我们提出了对KIVA燃烧软件开发的LES湍流模型的方法和结果,这是提高发动机内燃烧可预测性和效率的更大努力的一部分。在本研究中,LAU的Vreman动态LES方法[2012]在预测校正器分体(PCS)H自适应有限元方法(FEM)中实现,用于建模燃烧。 PCS H-Adaptive Fem模型实现了第二个和更高的空间精度,具有最小的计算工作量(Carrington等,[2013])。在我们的配方中,VREMAMN动态LES模型能够解决无任何壁阻尼功能或ad-hoc剪切的可压缩和不可压缩的流体流动,以防止不稳定(负)涡粘度,与SMAGORINSKY Supgrid模型(SM)不同。此外,它提供了在离散化中的实际误差的测量,并且可以调整空间精度,以最小化某些指定金额的错误。通过利用动态模型,可以将流动自动分类为流体或湍流,因为它的发展,提高了涡粘度的分辨率。目标是使用这种动态LES PCS HP-Adaptiveive FEM代码,称为Kiva-HPFE,用于在内燃机中发现的复杂几何形状的流动。在本文中,动态Vreman LES方法描述了关于质量,动量,能量和物种传输方程的离散化方案和SGS应力建模的简单几何形状。问题配置在后向步骤(BFS)上处理不稳定的湍流问题。以前的Carrington等[2013]的工作表明,Kivahpfe准确地捕获冲击和冲击波/边界层相互作用的能力,并且仿真与实验数据很好。在这项研究中,对后面的步骤的重新附点长度和瞬时流动与发布的模拟和实验数据相比。

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