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A Numerical method for steady linear waves due to a two-dimensional shallowly submerged hydrofoil

机译:二维浅埋水翼引起的稳定线性波的数值方法

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摘要

A design tool for predicting the flow past submerged hydrofoils is described, intended to give the designer guidelines in estimating efficiency of alternative hydrofoil configurations in motion at arbitrary Froude number below the free surface. A complete set of hydrodynamic characteristics may be evaluated, stored and represented by simple and exhaustive diagrams for each hydrofoil. The flow is simulated numerically by a finite number of singularities positioned along the foil's camber line. The exact free-surface boundary condition is replaced by a linearized condition since eventual inaccuracies in results may be not so relevant in many engineering applications. Numerical results of the performance characteristics are given for a NACA 16-012 symmetrical wing section which is particularly suitable for high-speed hydrofoil applications because of its low cavitation number.
机译:描述了一种用于预测流经浸没式水翼的流量的设计工具,旨在为设计人员提供指导,以估算在自由表面以下任意弗洛德数下运动的其他水翼构型的效率。可以评估,存储并通过每个水翼的简单且详尽的图表表示一整套水动力特性。通过沿箔的外倾线定位的有限数量的奇异点来数值模拟流动。精确的自由表面边界条件由线性条件代替,因为最终结果的准确性在许多工程应用中可能不那么重要。给出了NACA 16-012对称机翼截面的性能特征的数值结果,该截面特别适用于高速水翼应用,因为其空化数低。

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