The results indicated that it has a remarkable influence on ballistic effectiveness. Among properties, plastics and wave resistance are two major effect factors.
结果表明，背板材料的性能对其抗弹效益存在着较大的影响，其中塑性和波阻抗是两个主要影响因素。
The dynamic behavior of the liquid sloshing has great effect on the dynamic stability of the liquid filled space vehicle and the strategical ballistic missile.
液体推进剂的晃动特性对大型液体运载火箭以及战略弹道导弹的飞行动力稳定性有着很大的影响。
The dynamic behavior of the liquid sloshing has great effect on the dynamic stability of the liquid filled space vehicle and the strategical ballistic missle.
液体推进剂的晃动特性对大型液体运载火箭以及战略弹道导弹的飞行动力稳定性有着很大的影响。
This paper introduces the structural design, composition selection for G01 electric igniter and the effect of charge process on ballistic performance.
介绍了G01电点火具的结构设计、始发药、中间药和输出药的选择以及装药工艺对弹道性能的影响。
The effect of radial vibration of the chamber structure composed of propellant grain and case on the internal ballistic property of solid rocket motor (SRM) was investigated.
研究了由推进剂药柱和壳体组成的燃烧室结构径向振动对发动机内弹道性能的影响。
The basic structure, amplitude frequency response characteristics and ballistic deficit effect of the algorithm were studied with both theoretical analysis and computer simulation methods.
采用理论推导，结合数值模拟的方法，分析了梯形成形算法的基本结构、幅频特性以及弹道亏损。
At last, the effect on the outer ballistic trajectory characteristic after the ablation of hypersonic projectile wing has been analyzed.
最后，初步分析了高超声速弹翼表面发生烧蚀后对其外弹道特性的影响。
Emphasis of this simulation is on the flame-spreading process in the early interior ballistic cycle, especially on the effect of the radial flow on axial results.
本文模拟的重点是装药点燃初期火焰传播过程，特别是径向效应和它对轴向效应的影响。
The parameter' s effect to the interior ballistic character of the floating launch system was researched from theory aspect.
运用经典内弹道理论和内弹道气动力原理，建立了浮动发射系统的经典内弹道模型和气动力内弹道模型。
The results show that the inertial forces have less effect on deformation of ballistic spring within a limit range of rotation speed, and the deformation can be ignored.
分析表明，在通常转速范围内，旋转惯性力对弹道簧变形影响很小，可以忽略。
The low temperature sensitivity coefficient (LTSC) effect of high energy nitroamine propellant through the closed vessel and interior ballistic experiments is studied.
通过中止试验、高压密闭爆发器试验与火炮内弹道试验研究了低温感高能硝胺发射药的低温感效果。
The low temperature sensitivity coefficient (LTSC) effect of high energy nitroamine propellant through the closed vessel and interior ballistic experiments is studied.
通过中止试验、高压密闭爆发器试验与火炮内弹道试验研究了低温感高能硝胺发射药的低温感效果。
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