On condition that the front body shape of the projectile is unchangeable,a formula is obtained for determining the relation between the optimum boattail angle and the supersonic flight region.

 
  • 在彈丸前體外形和外界大氣密度不變的條件下,提出了利用彈丸炮口馬赫數和頂點(diǎn)馬赫數確定旋轉彈丸最佳尾錐角的方法。
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