对“控制水中层流边界层的分离:加热和吸力”一文的评论

A. Wortman
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引用次数: 1

摘要

将解析解应用于JEFF(A)的7/100比例模型,结果如图1所示。当弗劳德数为1.15时,将溶液归一化振幅的预测值(= IC l / a)与遇到频率和波长的关系绘制出来。波浪强迫项的大小和线性频率响应也分别显示,因为这些是产生起伏响应的因素。可以看出,飞行器的升沉响应是由波浪强迫曲线的形式控制的,而在此速度下,对于波长大于飞行器长度的预测线性频率响应是相当平坦的。为了进行比较,参考文献3中提出的拖曳箱试验中获得的实验确定的升沉响应包括在内。实验曲线的表现与理论预测大致相同。这表明,该模型可以用来解释物理机制和设计细节的影响,尽管不是精确的定量术语。
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Comments on "Controlling the Separation of Laminar Boundary Layers in Water: Heating and Suction'
The analytical solution has been applied to 7/100 scale model of the JEFF(A) with the results shown in Fig. 1. The predicted value of the normalized amplitude of the solution (= IC l / a ) is plotted vs encounter frequency and wavelength for a Froude number of 1.15. The magnitude of the wave forcing term and the linear frequency response are also shown separately since these are the factors which generate the heave response. It may be seen that the heave response of the vehicle is controlled by the form of the wave forcing curve, while the predicted linear frequency response is quite flat at this speed for wavelengths greater than the craft length. For comparison, an experimentally determined heave response obtained from towing tank tests as presented in Ref. 3 is included. The experimental curve behaves roughly in the same manner as the theoretical prediction. This suggests that the model may be relied upon to explain physical mechanisms and the influence of design particulars, though not in precise quantitative terms.
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