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Scale-Resolving Simulations with a Low-Dissipation Low-Dispersion Second-Order Scheme for Unstructured Flow Solvers

机译:非结构化流求解器的低耗散低色阶二阶方案的尺度解析仿真

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摘要

A new low-dissipation low-dispersion second-order scheme is applied to scale-resolving flow simulations using compressible and incompressible unstructured finite volume solvers. In wall-resolved and wall-modeled large-eddy simulations of the plane channel flow, the new scheme yields substantial improvements compared to the more dissipative/dispersive standard central scheme over a considerable range of Reynolds numbers. For general hybrid Reynolds-averaged Navier-Stokes/large-eddy simulations, a numerical blending approach is derived that uses a local sensor function to switch between the new scheme in the large-eddy simulation branch and the standard scheme in inviscid flow regions. After determining a suitable sensor formulation, the hybrid numerical scheme is applied to simulate a backward-facing step flow, for which satisfactory results and a reduced grid sensitivity are obtained. To demonstrate its potential in relevant aeronautical flows, the new scheme is successfully applied to hybrid Reynolds-averaged Navier-Stokes/large-eddy simulations of a three-element airfoil near stall and a rudimentary landing gear with massive flow separation.
机译:一种新的低耗散低色散二阶方案被应用到使用可压缩和不可压缩的非结构化有限体积求解器的水垢解析流动模拟中。在壁解析和壁建模的平面通道流动的大涡模拟中,与相当大的雷诺数范围内的耗散性/分散性标准中心方案相比,新方案产生了实质性的改进。对于一般的混合雷诺平均Navier-Stokes /大涡模拟,推导了一种数值混合方法,该方法使用局部传感器功能在大涡模拟分支中的新方案与无粘性流动区域中的标准方案之间进行切换。在确定合适的传感器公式后,将采用混合数值方案来模拟后向步进流,这样可以获得令人满意的结果和降低的网格灵敏度。为了展示其在相关航空流中的潜力,该新方案已成功应用于雷诺平均的Navier-Stokes /大涡模拟的失速附近的三元翼型和具有大流量分离的基本起落架。

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  • 来源
    《AIAA Journal》 |2016年第10期|2972-2987|共16页
  • 作者单位

    DLR, German Aerosp Ctr, Inst Aerodynam & Flow Technol, Bunsenstr 10, D-37073 Gottingen, Germany;

    DLR, German Aerosp Ctr, Inst Aerodynam & Flow Technol, Bunsenstr 10, D-37073 Gottingen, Germany;

    DLR, German Aerosp Ctr, Inst Aerodynam & Flow Technol, Bunsenstr 10, D-37073 Gottingen, Germany;

    DLR, German Aerosp Ctr, Inst Aerodynam & Flow Technol, Bunsenstr 10, D-37073 Gottingen, Germany;

    DLR, German Aerosp Ctr, Inst Aerodynam & Flow Technol, Bunsenstr 10, D-37073 Gottingen, Germany;

  • 收录信息 美国《科学引文索引》(SCI);美国《工程索引》(EI);
  • 原文格式 PDF
  • 正文语种 eng
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