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Development of numerical schemes for the fluid flows with accurate boundary condition

Development of numerical schemes for the fluid flows with accurate boundary condition
开发具有精确边界条件的流体流动数值方案
批准号:
10440028
负责人:
ISHII Katsuya
金额:
$5.44万
依托单位:
依托单位国家:
日本
项目类别:
Grant-in-Aid for Scientific Research (B)
财政年份:
1998
资助国家:
日本
项目状态:
已结题
起止时间:
1998 至 1999

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中文摘要
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英文摘要
The Purpose of this study is to develop high accurate numerical schemes for the fluid flow by using the accurate boundary conditions. For the simulation of the fluid flow, the adequate choice of numerical boundaries and/or interfaces is needed. We considered three numerical problems : (A) the fluid flow with three dimensional free surface or interface, (B) the boundary conditions of the vortical flow field interacting with acoustic waves, and (c) the boundary conditions of the vortical flow field interacting with acoustic waves. and (c) the boundary conditions for the scheme with accuracy and high resolutions. The results of the study are as follows :(1) The level set formulation for the interface of two-phase fluids is developed in the three-dimensional incompressible flow calculations, including large density and viscosity ratio as well as surface tension effects. Numerical simulations carried out for two rising gas bubbles, the interaction of buoyant drops with a fluid-fluid interfa … More ce, and the propagation of surface waves. The results agree with previous experiment data, and make it possible to analyze the physical quantities near the boundaries.(2) Improving the boundary conditions for the vector velocity potential, we get the accurate numerical method for the localized vorticity fields. Using this method, the vortex sounds can be evaluated in the various flow fields, and the sound generation mechanism can be analyzed.(3) Using the no reflective boundary conditions, the acoustic control of flow separation at low Reynolds numbers are studied. We reproduced the phenomena that the tendency toward the separation on an airfoil is reduced by an acoustic excitation, and analyze the detailed flow field near the point of separation.(4) The combined compact scheme with high accuracy and high resolution is developed in the generalized grid system with concentrated points near the boundary. This scheme gives more accurate numerical results compared with the other finite difference methods. Less
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通讯作者:
Suzuki, S.: "Numerical Analysis of the Separation on a 2-D Airfoil by Acoustic Excitation"to appear in Computational Fluid Dynamics J.. (2000)
Suzuki, S.:“通过声学激励对二维翼型件进行分离的数值分析”出现在《Computational Fluid Dynamics J.》(2000 年)中
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Kaneda, Y.: "Taylor Expansions in Power of Time of Lagrangian and Eulerian Two-Point Two-Time Velocity Correlations in Turbulence"Phys. Fluids. 11. 2154-2166 (1999)
Kaneda, Y.:“湍流中拉格朗日和欧拉两点两次速度相关性的时间幂的泰勒展开式”物理学。
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21
    Study of a 3D Cavity Flow using the Numerical Scheme with High Accuracy
    • 批准号:
      21540383
    • 项目类别:
      Grant-in-Aid for Scientific Research (C)
    • 资助金额:
      $2.83万
    • 财政年份:
      2009
    • 负责人:
      ISHII Katsuya
    • 依托单位:
    Research on a highly accurate parallel numerical methods for fluid equations with portability
    • 批准号:
      16605004
    • 项目类别:
      Grant-in-Aid for Scientific Research (C)
    • 资助金额:
      $2.43万
    • 财政年份:
      2004
    • 负责人:
      ISHII Katsuya
    • 依托单位:
    海外基金