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首页> 外文期刊>Journal of Aerospace Sciences and Technologies >AN ALTERNATIVE REYNOLDS SHEAR STRESS MODEL AND WAKE MODEL FOR A FLAT PLATE BOUNDARY LAYER FLOW
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AN ALTERNATIVE REYNOLDS SHEAR STRESS MODEL AND WAKE MODEL FOR A FLAT PLATE BOUNDARY LAYER FLOW

机译:平板边界流的交替雷诺剪切应力模型和尾流模型。

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摘要

The well-known closure problem has led to many models for the Reynolds shear stress. But many of these models are based on the Boussinesq approximation involving the mean velocity gradient and an eddy viscosity, which, however, requires to be modeled. Here, for a steady, incompressible and constant-pressure boundary layer, the Reynolds shear stress is expressed as a product of the mean velocity and the local momentum-deficit. This closure model is then incorporated in the boundary layer equation for the outer layer to predict the streamwise velocity in the wake region.
机译:众所周知的闭合问题导致了雷诺剪切应力的许多模型。但是,这些模型中的许多模型都是基于Boussinesq逼近法,其中涉及平均速度梯度和涡流粘度,但是需要对它们进行建模。在此,对于稳定,不可压缩且恒压的边界层,雷诺剪切应力表示为平均速度和局部动量赤字的乘积。然后将此封闭模型合并到外层的边界层方程中,以预测尾流区域的水流速度。

著录项

  • 来源
    《Journal of Aerospace Sciences and Technologies 》 |2019年第4期| 365-377| 共13页
  • 作者

    P. Phani Kumar; J. Dey;

  • 作者单位

    Department of Aerospace Engineering GITAM Institute of Technology Hyderabad India;

    No. 451 Tatanagar Bangalore-560 092 India Formerly at Department of Aerospace Engineering Indian Institute of Science Bangalore-560 012 India;

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  • 正文语种 eng
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