The oblique detonation stabilized on a hypervelocity projectile was researched by numerical simulations and experimental visualizations.
通过数值模拟和实验显示的方法对驻定在高速飞行体上斜爆轰波流场进行研究。
The range equipment for the investigation of the hypervelocity aerodynamic properties and flow field of explosively formed projectile(EFP) models is described.
本文描述的是研究爆炸成型发射弹（EFP）模型的流场及超高速空气动力特性所用的弹道试验设备；
This paper describes in detail the technology used in the separation of projectile from its seat in the hypervelocity impact study on the two-stage light gas gun.
本文详细介绍了利用二级轻气炮发射超高速弹丸的弹托分离技术。
This paper describes in detail the technology used in the separation of projectile from its seat in the hypervelocity impact study on the two-stage light gas gun.
本文详细介绍了利用二级轻气炮发射超高速弹丸的弹托分离技术。
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