平底模型船下气液两相湍流边界层中空穴波的发展

Taiji Tanaka, H. Park, Y. Tasaka, Y. Murai
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引用次数: 0

摘要

为了研究空泡波的发展过程和空泡分数的时空波动,我们对一个有气泡注入的湍流边界层进行了实验研究。实验是在一个4米长的透明模型船的平底上进行的,拖曳在100米长的水箱中,速度高达3.00米/秒。在等速气泡注入中,随着拖曳速度的变化,出现了4 Hz或8 Hz的空隙波动。在气流流速周期性波动的情况下,在湍流边界层中提供人工空洞波,并在下游传播过程中保持其频率。在特定注入频率条件下,用傅里叶分析评估的波动衰减率取最小值。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Void Waves Developing in Gas-Liquid Two-Phase Turbulent Boundary Layers Beneath a Flat Bottom Model Ship
To investigate the development process of a void wave, spatio-temporal fluctuation of void fraction, we examined experimentally a turbulent boundary layer with bubble injections. The experiments performed on a flat bottom of 4-mlong transparent model ship towed in a tank of 100 m length with the speed of up to 3.00 m/s. In bubbles injection with constant air flow rate, void fluctuations with 4 Hz or 8 Hz appeared dependent on the towing speed. With periodically fluctuated air flow rate, artificial void waves were provided into the turbulent boundary layer and their frequency was maintained during the downstream propagation. The attenuation rate of the fluctuation evaluated using Fourier analysis of the wave took the minimum value at specific injection frequency conditions.
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