水下射弹自然超空泡减阻特性的数值模拟

NUMERICAL SIMULATION ON DRAG REDUCTION OF NATURAL SUPERCAVITATION INDUCED BY UNDERWATER PROJECTILE

  • 摘要: 基于均质平衡多相流理论,采用Fluent6.3对水下射弹自然超空泡减阻特性进行了数值模拟。研究了空化数对水下射弹空泡闭合部位和阻力系数的影响,重点分析了水下射弹结构参数对自然超空泡减阻特性的影响,得到了空化器直径、模型长细比和不同尾部形状对水下射弹超空泡减阻特性影响的规律。数值模拟结果表明:随着空化器直径的增大,自然超空泡较易形成,但其减阻能力有所降低;随着长细比的增大,自然超空泡较难形成,但形成超空泡后,不同长细比模型的阻力系数基本一致;尾部形状只影响尾部空泡的发展过程,当尾部被空泡包裹后,模型的自然超空泡形态和阻力系数基本一致。

     

    Abstract: The drag reduction characteristic of the underwater projectile natural supercavitation was simulated based on the homogeneous equilibrium multiphase theory through using commercial CFD Code FLUENT6.3. The effects of the cavitation number on the location where the cavity of the underwater projectile is closed to and the variation of the drag coefficient are numerically investigated. The effect of the structure parameters of the underwater projectile on the drag reduction characteristics of natural supercavitations is analyzed. The effects of the cavitator diameter, the aspect ratio and different shapes of the afterbody on the drag reduction characteristics of the underwater projectile natural supercavitation were found. The results of the numerical simulation show that: with the diameters of the cavitator increased, the natural supercavitation formed easily, but the capability of the natural supercavitation decreased to some extent. The natural supercavitation came into being hardly as aspect ratio increased, and almost the same that the drag coefficient of a different aspect ratio model was. The development of the cavity induced by different afterbodies was only affected by its shape. The variations of the natural supercavitation’s shape and that of the drag coefficients of different shapes of afterbodies are almost the same as long as the afterbody are covered all over by the cavity.

     

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