一种适用于面穿水翼和螺旋桨的数值计算公式

C. Savineau, S. Kinnas
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引用次数: 17

摘要

研究了任意几何形状的完全通风二维水翼的流场。提出的理论是一种非线性的、时间推进的、基于势的边界元方法。空腔上的微扰势是浸入和时间的函数。在每个时间步长的解内迭代确定非线性空腔的几何形状。利用“负像”方法实现了无限弗劳德数下的线性化自由曲面条件。所开发的分析表明,收敛良好的迭代每时间步,即使空腔几何已被发现是敏感的面板布置在箔前缘。在小迎角时,压力分布与线性化的分析结果比较好,但在大迎角时,非线性效应是明显的。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
A Numerical Formulation Applicable to Surface Piercing Hydrofoils and Propellers
The flow field around a fully ventilated two-dimensional hydrofoil of arbitrary geometry is considered. The presented theory is a non-linear, time marching, potential based boundary element method. The perturbation potential on the cavity is a function of submergence and time. The non-linear cavity geometry is determined iteratively within the solution at each timestep. A linearized free surface condition, at infinite Froude number, is enforced by using the “negative image” approach. The developed analysis is shown to converge well with iterations per timestep, even though the cavity geometry has been found to be sensitive to the panel arrangement at the foil leading edge. Pressure distributions compare very well with linearized analytical results at small angles of attack, but the non-linear effects are noticeable at larger angles of attack.
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