无控滑翔子弹的气动设计

Aerodynamic Design of Unguided Glider Submissiles

  • 摘要: 采用理论与实验相结合的方法进行了滑翔子弹的气动外形设计。风洞试验结果表明,尾翘确有使子弹滑翔的作用。所采取的3项预防滚转措施显著地减小了卷弧翼的滚转力矩。弹道仿真结果表明,滑翔子弹的飞行距离约比常规尾翼子弹增大了80%,可以有效地扩大子弹的撒布范围

     

    Abstract: The idea of aerodynamic design for an unguided glider submissile is introduced. Wind tunnel experimental results indicate that the tail raiser plays the role of causing a submissile to glide.The three measures adopted to prevent rolling remarka-bly decrease the moment of rolling in wrap-around wings and /or fins.The results of trajectory simulation show that the flying distance of glider submissile has increased for approximately 80% when compared with normalfinned submissiles. It may effectively extend the scope of throw of submissiles.

     

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