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Numerical simulation of flow around two- and three-dimensional partially cavitating hydrofoils

机译:二维和三维局部空化水翼绕流的数值模拟

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摘要

A new method is developed for the prediction of cavity on two-dimensional (2D) and three-dimensional (3D) hydrofoils by a potential-based Boundary Element Method (BEM). In the case of specified cavitation number and cavity length, the iterative solution method proceeds by addition or subtraction of a displacement thickness on the cavity surface of the hydrofoil. The appropriate cavity shape is obtained by the dynamic boundary condition on the cavity surface and the kinematic boundary condition on the whole foil surface including the cavity. For a given cavitation number the cavity length of 2D hydrofoil is determined according to the minimum error criterion among different cavity lengths. In the 3D case, the prediction of cavity is exactly the same as in the case of 2D method in span wise locations by the transformation of the pressure distribution from analysis of 3D to 2D. The 3D effects at each span-wise location are considered by the multiplication of the cavitation number by a coefficient. The pressure recovery and termination wall models are used as cavity termination. For the 2D case the NACA 16006 and NACA 16012 hydrofoil sections are investigated for two angles of attack using different cavity termination models. For 3D analysis an application for a rectangular hydrofoil with NACA16006 section is carried out. The results are compared with those of other potential based boundary element codes and a commercial CFD code (FLUENT). The effects of different Reynolds numbers (R_n) on the cavitation behavior are also investigated. The results developed from present method are in a good agreement with those obtained from the others.
机译:通过基于势的边界元方法(BEM),开发了一种用于预测二维(2D)和三维(3D)水翼上空腔的新方法。在指定的气蚀次数和腔长的情况下,迭代求解方法是通过在水翼的腔表面上增加或减去位移厚度来进行的。通过在腔表面上的动态边界条件和在包括腔在内的整个箔片表面上的运动学边界条件来获得合适的腔形状。对于给定的气穴数,根据不同腔体长度之间的最小误差标准确定二维水翼的腔体长度。在3D情况下,通过将压力分布从3D分析转换为2D,在跨度位置上的腔体预测与2D方法的情况完全相同。通过将空化数乘以系数来考虑每个跨度位置的3D效果。压力恢复和端接壁模型用作腔体端接。对于2D情况,使用不同的腔终止模型研究了NACA 16006和NACA 16012水翼型材的两个迎角。对于3D分析,将应用NACA16006截面的矩形水翼。将结果与其他基于势能的边界元素代码和商业CFD代码(FLUENT)的结果进行比较。还研究了不同的雷诺数(R_n)对空化行为的影响。从本方法获得的结果与从其他方法获得的结果非常一致。

著录项

  • 来源
    《Ocean Engineering》 |2014年第1期|22-34|共13页
  • 作者单位

    Yildiz Technical University, Department of Naval Architecture and Marine Engineering, 34349 Besiktas, Istanbul, Turkey;

    Yildiz Technical University, Department of Naval Architecture and Marine Engineering, 34349 Besiktas, Istanbul, Turkey;

    Istanbul Technical University, Department of Naval Architecture and Marine Engineering, 34469 Maslak, Istanbul, Turkey;

  • 收录信息
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

    Boundary element method; Sheet cavitation; CFD; Hyrofoil; Cavity termination model;

    机译:边界元法;气蚀现象差价合约水翼腔终止模型;

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