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INVESTIGATIONS ON THE DRAG REDUCTION OF HIGH-SPEED NATURAL SUPERCAVITATION BODIES

机译:高速自然超空机构的减阻研究

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In order to investigate the drag reduction characteristics of a high-speed body with supercavitation shape, four types of typical disk cavitator models with different parameters were designed and tested. By measuring the velocity decrease histories during supercavitating flow experiments, the average drag coefficients were determined, which allows analysis and comparison of the influence of cavitator diameter, projectile aspect ratio, and cavitation number on the drag reduction . Based on the experimental results, numerical simulation of the drag reduction of supercavitation body was also carried out using a commercial software FLUENT6.2, and the results obtained agree well with the experimental data. Moreover, it is shown that the drag coefficients of the four bodies are in inverse ratio to the head area of cavitator when operating under natural supercavitating flow condition, and the smaller drag coefficient can be obtained by increasing the slender ratio of the bodies. Therefore, higher aspect ratio reduces drag coefficient, with the reduction of more than 95% under certain condition of cavitation number and supercaviation shape.
机译:为了研究具有超空化形状的高速物体的减阻特性,设计并测试了四种具有不同参数的典型圆盘空化器模型。通过测量超空化流动实验中的速度下降历史,可以确定平均阻力系数,从而可以分析和比较空化器直径,弹丸纵横比和空化数对减阻的影响。根据实验结果,还使用商业软件FLUENT6.2对超空化体减阻进行了数值模拟,所得结果与实验数据吻合良好。而且,显示了当在自然超空化流动条件下操作时,四个主体的阻力系数与空化器的头部面积成反比,并且可以通过增加主体的细长比率来获得较小的阻力系数。因此,较高的长宽比可降低阻力系数,在一定的空化数和超空化形状的条件下可降低95%以上。

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