航空学报 > 1999, Vol. 20 Issue (2): 152-154

近壁湍流相干结构的数值模拟

陆昌根   

  1. 南京航空航天大学六系, 南京, 210016
  • 收稿日期:1998-05-20 修回日期:1998-10-09 出版日期:1999-04-25 发布日期:1999-04-25

NUMERICAL SIMULATION OF COHERENT STRUCTURE IN THE WALL REGION OF TURBULENT FLOW

Lu Changgen   

  1. Dept.of Aerodynamics, Nanjing University of Aeronautics and Astronautics, Nanjing, 210016
  • Received:1998-05-20 Revised:1998-10-09 Online:1999-04-25 Published:1999-04-25

摘要:

提出了近壁湍流对称单个相干结构的理论模型,采用紧致有限差分和Fourier谱展开相结合的数值方法研究它的演化问题,得到雷诺应力分布及高剪切层的形成过程与实验结果一致。

关键词: 近壁湍流, 数值模拟, 单个相干结构

Abstract:

In the paper, the three dimensional,time dependent,incompressible Navier Stokes equations are numerically solved by the compact finite difference and Fourier spectral hybrid method.A third order mixed explicit implicit fractional step scheme is here employed for the time discretization.The space discretization is implemented using the Fourier spectral expansion and high order compact finite differences.A theoretical model of the symmetric single coherent structure in the wall region of turbulent flow is proposed,utilizing the idea of resonant triad in the theory of hydrodynamic stability.The evolution of the model is numerically studied by the numerical method.The obtained Reynolds stress distribution and the process of the formed strong shear layer are in reasonable agreement with experimental results.

Key words: the wall r egion of t ur bulent flow, numer ical simulation, single coher ent structur e

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