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Investigations on the accurate prediction of supersonic shear layers for detached eddy simulation

机译:用于分离涡仿真的超音速剪切层精确预测的研究

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摘要

One of the current problems of the detached eddy simulation (DES) and delayed DES (DDES) methods is the inaccuracy in prediction of the separated shear layer flows, which mainly reflects in the delayed development of the shear layer. To correctly simulate the separated shear flow, various modified definitions of the DDES length scale are investigated and the improved definition of the subgrid eddy viscosity is introduced to deal with the delayed development problem for the first time. In this paper, the shear layer without the upstream boundary layer is studied in order to assess the subgrid model of the DDES in the simulation of shear layers. Large eddy simulation (LES) and experiment results are introduced to test the performance of different definitions of the DDES parameters. According to the results, both the definitions of the length scale and subgrid eddy viscosity coefficient should be improved to get the best prediction. DDES with the LES length scale and vorticity-correlated length scale as well as the modified definition of the subgrid eddy viscosity coefficient predict a more accurate development of the shear layer than DDES with the original definitions, which provides a possible solution to the delay development problem of the shear layer. Furthermore, the LES mode of DDES performs considerably differently from the Smagorinsky-LES, which shows the former subgrid model is essentially different from that of Smagorinsky-LES. Theoretical analyses are made in order to find out the quantitative difference of the subgrid eddy viscosity between the LES mode of DDES and Smagorinsky-LES. (C) 2019 Elsevier Masson SAS. All rights reserved.
机译:分离的涡流模拟(DES)和延迟DES(DDES)方法的目前问题之一是在分离的剪切层流动预测中的不准确,其主要反映剪切层的延迟显影。为了正确模拟分离的剪切流,研究了DDES长度尺度的各种修改定义,并引入了亚耕楦粘度的改进定义,首次处理延迟的发育问题。在本文中,研究了没有上游边界层的剪切层,以评估剪切层模拟中DDES的底图模型。引入大涡模拟(LES)和实验结果,以测试DDES参数的不同定义的性能。根据结果​​,应该改善长度尺度和亚底涂层粘度系数的定义以获得最佳预测。具有LES长度和涡旋相关长度的DDES以及子涡流粘度系数的修改定义预测剪切层比具有原始定义的DDE更准确地开发剪切层,这为延迟发育问题提供了可能的解决方案剪切层。此外,DDE的LES模式与SMAGORINSKY-LES相当不同,其示出了前者模型基本上与SMAGORINSKY-LES的模型不同。制备理论分析,以便在DDES和Smagorinsky-LES的LES模式之间找出亚底涂层粘度的定量差异。 (c)2019年Elsevier Masson SAS。版权所有。

著录项

  • 来源
    《Aerospace science and technology》 |2019年第6期|46-57|共12页
  • 作者单位

    Beihang Univ Sch Aeronaut Sci & Engn Natl Lab Computat Fluid Dynam Beijing 100191 Peoples R China;

    Beihang Univ Sch Aeronaut Sci & Engn Natl Lab Computat Fluid Dynam Beijing 100191 Peoples R China;

    Beihang Univ Sch Aeronaut Sci & Engn Natl Lab Computat Fluid Dynam Beijing 100191 Peoples R China;

    Beihang Univ Sch Aeronaut Sci & Engn Natl Lab Computat Fluid Dynam Beijing 100191 Peoples R China;

    Beihang Univ Sch Aeronaut Sci & Engn Natl Lab Computat Fluid Dynam Beijing 100191 Peoples R China;

    Beihang Univ Sch Aeronaut Sci & Engn Natl Lab Computat Fluid Dynam Beijing 100191 Peoples R China;

  • 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
  • 中图分类
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