水中弹药引信外置涡轮高速旋转两相流动数值仿真

Numerical simulation of high-speed rotation two-phase flow for underwater ammunition fuze external turbine

  • 摘要: 为预测空化条件下的涡轮转速,获得涡轮叶片附近空化情况、压力系数、阻力系数等数据,采用Schnerr-Sauer空化模型,进行了水中弹药引信涡轮高速旋转两相流动的三维流场数值仿真研究。计算得到不同水深(10m、30m及50m)和弹速(5~100m/s)条件下的流场数据。结果表明:引信涡轮表面在弹速30m/s左右时空化初生,且空化尺度随着弹速的增加而增大;弹速100m/s时,头部粘性阻力占总阻力的18.7%;涡轮转速与水深、静压、弹速相关,高速时涡轮转速随水深减小明显,与弹速基本成正比线性关系,非线性度约为0.998。

     

    Abstract: In order to predict turbine rotation speed under the conditions of cavitation, obtain hydrodynamic performance data such as cavitation situation nearby turbine blades, pressure coefficient of turbine hub surface and drag coefficient of the projectile, the two-phase three dimensional flow field was investigated by numerical simulation method for underwater ammunition fuze turbine with high rotation speed. Schnerr and Sauer cavitation model was adopted, and the flow field data under different depths (10m, 30m and 50m) and projectile velocitiy (5~100m/s) conditions were obtained. The results showed that fuze turbine surface cavitation start to occur near the projectile velocity of 30m/s, and with the increment of velocity, cavitation scale increased. When the projectile velocity is 100m/s, the head viscous drag is about 18.7% of the total drag. The turbine rotation speed is related to the depth of water, static pressure and projectile velocity. The turbine rotation speed decreases significantly with depth of water at high projectile speed, and there has nearly a linear relationship between the turbine speed and projectile velocity, non-linearity of which is about 0.998.

     

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