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1)  terminal ballistics
终点弹道
1.
Numerical Simulation on Projectile s Terminal Ballistics;
弹头终点弹道的数值模拟研究
2.
Based on a comprehensive study of the effect of flared EFP shape parameters on the aerodynamic performance and terminal ballistics, a new optimized design that is engineering achievable at present is presented, in order to reduce flight drag and improve flight stability, and thus to increase the depth of penetration of the EFP.
本文针对常规EFP的飞行阻力大、稳定性差的缺点 ,以提高其侵深为目标 ,在综合研究轴对称裙式EFP弹形参数对气动性能及终点弹道影响规律的基础上 ,提出一种新的具有工程实现可能性的EFP气动优化方案 :对于前体 ,根据杆式头部破甲弹的气动原理 ,通过增加一尖锥 ,改善其气动特性 ;对后体 ,仍采用简便的裙式 ,优化裙体参数。
3.
This paper investigated the concept of the danger area in firing experiment and combining exterior ballistics, media ballistics and terminal ballistics theories, provided models and calculation methods using in the calculation and the make up of danger area model.
利用射击试验危险区的概念,结合外弹道、终点弹道和(土壤)介质弹道的理论,提出了关于射击实验危险区样板制作的模型和计算方法,并据此进行了实例计算。
2)  terminal ballistics
终点弹道学
1.
According to the terminal ballistics theory,the damage theory and the explosion theory,and on the bases of analyzing bomb\'s explosive rule,fragment\'s flight rule and the damage to fighter by fragment,this paper puts forward a method of evaluating the secure distance of draw back and the secure altitude when it is in the process of bombing horizontally in low altitude.
根据终点弹道学理论、毁伤理论和爆炸理论,在分析炸弹的爆炸规律、破片的飞行规律及破片对战斗机毁伤作用的基础上,提出了低空水平轰炸过程中安全退曳距离及安全高度的估算方法。
3)  ballistic limit
终点弹道极限
1.
Analytical formulae for the perforation ballistic limit and the residual velocity are obtained for a range of p.
进一步发展了考虑结构响应的剪切冲塞模型,计及前舱物的作用,对带前舱物的钝头弹穿甲金属靶的工程问题进行了刚塑性分析,用于分析终点弹道极限和剩余速度。
4)  terminal ballistic experiment
终点弹道试验
5)  terminal ballistic effect
终点弹道性能
1.
Influence of detonation driving on terminal ballistic effects of tungsten spheres;
爆轰驱动对钨珠终点弹道性能的影响
6)  endgame [英]['endɡeɪm]  [美]['ɛnd'gem]
弹道终端
1.
The process of image tracking for the endgame was first analyzed, then a model of perspective projection for the imaging detector was provided.
弹道终端目标图像充满视场时的跟踪点选择和继续跟踪能力是第四代先进空空导弹必须具备的性能。
2.
The reason of blind area generation during endgame was analyzed and the approach of blind area reduction through partial image tracking algorithm was proposed,the principle of tracking position selection for aircraft was discussed.
分析了弹道终端红外成像导引头跟踪盲区形成的原因,提出了采用局部图像跟踪算法减小跟踪盲区的思想,讨论了飞机目标局部图像跟踪部位的选取原则。
补充资料:终点弹道学
终点弹道学
terminal ballistics
    见弹道学。
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