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离散杆战斗部杆条飞行性能模拟试验研究
Simulated Experiment on Flight Performance of Rod about Discrete Rod Warhead
【摘要】 通过离散杆战斗部靶场静爆试验,对离散杆式破片的飞行性能进行了试验研究。试验结果表明:采用波形控制器可以较好地控制战斗部爆炸后杆形破片的飞散方向,以及保证杆条的完整率;杆条的飞行姿态与放置角有密切关系,主要通过杆条旋转速度表现出来。
【Abstract】 Through the exploding experiment of discrete rod warheads at shooting range, the flight performance of the rods about discrete rod warheads is researched. The experimental results show that the wave shaper can control the moving direction of the rod fragments after the warheads exploded and ensure the integrity rate of the rod and that there is a close relationship between the flight attitude and the positioned angle , which is mainly reflected by the rotation velocity of the rod.
- 【文献出处】 南京理工大学学报(自然科学版) ,Journal of Nanjing University of Science and Technology(Natural Science) , 编辑部邮箱 ,2006年05期
- 【分类号】TJ410.6
- 【被引频次】5
- 【下载频次】188