简易控制远程多管火箭密集度仿真是提高射击密集度和减少简易制导多管火箭试验用弹量的重要手段。
It is very important to simulate the precision of fire of simple control Long Range Multiple Launch rocket System (LRMLRS) for improving the dispersion and reducing the number of rocket used in test.
用氧弹式量热计测定液态烃燃料的燃烧热值的测试方法05。
Heat of Combustion of Liquid Hydrocarbon Fuels by Bomb Calorimeter, Method of Test for 05.
岩心试验中还研究了岩心渗透率和溶液含盐量对粘弹流动的影响。
The effect of core permeability and solution salinity on viscoelastic flow has also been studied.
以拦截弹在视线系z向上的脱靶量达到最大值作为性能指标，对机动发动机开启时刻进行优化确定。
Taking miss distance of the interceptor along line-of-sight Z direction as performance index, start-up time of the motor w.
给出了超环面行星蜗杆传动啮合效率、齿面磨损量和弹流油膜厚度的分布规律及其随传动参数的变化规律。
The distribution of engaging efficiency, EHD oil film thickness and tooth face wear and their changes along with transmission parameters are presented.
采用全量理论和幂级数形式的应力一应变曲线，导出了弹塑性强化材料旋转园盘的渐近解。
Based on the stress - strain curve uith Power series, the asymptotic nalytical solution of rotating disks uith strain-hardening is obtained from the total strain theory.
分析了母弹的射击误差、子弹的散布误差、目标幅员、重迭度、子弹携带量及射距离对子母弹首发命中概率的影响。
Influences on the hitting probability by error of carrier, by dispersion of sub-projectiles, by size of target, by the Numbers of sub-projectiles, and by the range of fire are analyzed.
根据弹塑性有限元理论，利用有限元软件建立了切削模型，得到了不同切削速度和进给量下已加工工件的残余应力。
Acording to elastoplasticity FEM, cutting models are created and the residual stress of workpieces machined with different cutting speed and feed are obtained in this article.
计算结果表明，漏流涡对叶片气弹稳定性影响较大，大涡量的漏流涡能抑制叶片颤振发生。
The results show that the tip leakage flow vortex has a great effect on the blade aeroelastical stability and large tip leakage vorticity may restrain blade flutter.
论述了采用某导弹战斗弹遥测系统中的“视频遥测”信号推算导弹靶试时脱靶量的原理，介绍了两种处理脱靶量的方法。
Describes the principle of miss distance assessing by using video TLM in one missile's video pack telemetry system, and introduces two methods of miss distance assessing.
分析了不同脱靶角和不同脱靶量弹目交会信号；
An analysis of results in various miss distance and miss azimuth was made.
流体注入压力越高，热弹变形量越大，密封端面平衡间隙亦越大。
A higher pressure of the inlet fluid will result in the increases of thermo-elastic deformation and the balancing film thickness.
方法采用量热法，利用氧弹式量热计对青海产枸杞进行热值测定。
Method Calorific value of Qinghai matrimony-vine was determined by the method of oxygen bomb type-calorimeter instrument.
方法采用量热法，利用氧弹式量热计对青海产枸杞进行热值测定。
Method Calorific value of Qinghai matrimony-vine was determined by the method of oxygen bomb type-calorimeter instrument.
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