轴对称航行体通气超空泡的特性实验研究

EXPERIMENTAL INVESTIGATION OF VENTILATED SUPERCAVITY ON SYMMETRICAL UNDERWATER BODIES

  • 摘要: 为了研究超空泡的减阻效果,保证在较低流速下生成超空泡,在水洞中开展了水下航行体通气超空泡的实验研究。采用通气的方法在较低水速下(V= 7m/s-15m/s)生成人工通气超空泡,通过改变通气率和弗洛德数,获得了不同条件下通气空泡的长度,给出了不同空泡长度下的模型阻力系数。研究结果表明,来流速度不变时,空泡长度随通气率的增加而增加,阻力系数随空泡长度的增加先递增后递减;重力场造成了空泡形态的严重不对称,通过比较模型上下表面的空泡长度,定量的给出了弗洛德数对通气空泡长度的影响。当Fr >43.74时,重力场对通气空泡长度的影响几乎可以忽略。

     

    Abstract: In order to form supercavity at lower velocity and explore drag reduction by supercavity, experiments of ventilated supercavity on symmetrical underwater bodies have been performed in water tunnel. Supercavity has been formed by using ventilation method at lower velocity. By changing ventilation volume and Froude number, different supercavity lengths and corresponding drag coefficients of model have been obtained. Experimental results show that supercavity length increases with ventilation coefficient increasing at constant velocity. Drag coefficient of model reduces initially and then begins to increase slowly as the cavity length increases. Gravity causes strong asymmetry of ventilated supercavity. By comparing supercavity length of upper wall with that of lower wall, the influence of Froude number on ventilated supercavity length has been quantified. The influence can be ignored at Fr >43.74.

     

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