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1)  truncated-ogive-nose projectile
截卵弹丸
1.
In this paper,to build the analytical model of truncated-ogive-nose projectile piercing armor,the ogive- nose projectile is build based on the conventional model and great of numerical simulation.
针对典型截卵弹丸的穿甲参数计算,将截卵弹丸头型分解为平头、直锥、尖卵头型,基于传统的穿甲计算解析模型,以部分文献试验结果为参照。
2)  ogival-nosed projectiles
卵形弹丸
1.
Penetration and perforation of FRP laminates under normal impact by ogival-nosed projectiles;
卵形弹丸撞击下FRP层合板的侵彻和穿透
3)  cone-cylinder projectile
变截面弹丸
4)  ogive-nose projectile
卵形头部弹丸
5)  projectiles [英][prə'dʒektil]  [美][prə'dʒɛktɪl]
弹丸
1.
In regard to acquire the attitude of flying projectiles using velocity measurement radar with linear polarization antenna, a characteristic parameter was deduced and analyzed based on polarization theory by slotting at the bottom.
针对用线极化天线测速雷达测量弹丸飞行姿态问题,利用电磁理论推导并分析了底部刻槽弹丸的姿态特征参数。
2.
With zonal patched grid technology and second-order zonal solver method,the numerical simulation on inlet complex flow field of solid rocket ramjet assisted range projectiles with different struts shapes was made at different Mach!numbers.
结合分区对接网格技术和二阶精度区域分解算法,对某冲压增程弹丸进气道在不同来流攻角和不同侧向支柱形状工况下的内外复杂流场进行了数值模拟。
3.
Applied block structure grid and second-order zonal solver method,the numerical simulation on supersonic inlet complex flow field of solid rocket ramjet assisted range projectiles with struts was presented.
采用块结构网格与二阶精度流场分区求解技术,对含侧向支柱冲压增程弹丸进气道内外复杂流场进行了数值模拟。
6)  projectile [英][prə'dʒektaɪl]  [美][prə'dʒɛktḷ]
弹丸
1.
The principle for measuring motion parameters of projectiles using two sky screens in vertical intersection manner;
双天幕靶交汇测量弹丸飞行参数原理
2.
Numerical Simulation of Projectile Explosion Process;
弹丸爆炸过程的数值模拟
3.
The Investigation on Perforation Mechanism of Different Nose Shape Projectiles Impacting Thin Steel Target;
不同头形弹丸对薄钢靶的穿甲机理研究
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