喷流对航空器荷电影响的研究

Influence of Plume Flow on Aerostats Charging Properties

  • 摘要: 为了研究喷流中带电粒子对航空器荷电的影响,通过建立喷流中的荷电数学模型和某型导弹的喷流几何模型,采用仿真的方法对喷流对航空器荷电的影响进行了分析. 仿真结果表明,喷流对航空器的荷电影响主要集中在航空器的尾翼和喷嘴处,喷流中碳黑粒子的粒径及其荷电量对航空器的荷电量和极性均有一定影响.

     

    Abstract: To study the influence of plume flow on aerostats charging, mathematical model of the plume flow and geometric model of some type of guided missiles are established, and plume flows effects on some type of guided missiles charging properties are analyzed with the help of simulation. The results indicated that plume flows effects on aerostats charging concentrate on the tail fin and nozzle, the particle diameter and charge of the soot carbon particle influence on aerostats charge quantity and polarity.

     

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