弹翼 meaning in Chinese
missile wing
Examples
- An profile evaluating method based on least square principle is described
在该系统中给出了一种基于最小二乘原理的弹翼轮廓误差评价方法。 - 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。 - To overcome the shortcomings of low efficiency and high uncertainty in the measurment of wings ' cross section shape by using a templet , a nc non - contact measuring system is designed
摘要为解决使用专用样板进行弹翼测量效率低、误检率高的缺点，设计了一种数控非接触测量系统。 - The model is solved with the finite difference method , the simulation software is organized to simulate the transient thermal response of the front region of projectile wing such as those launched by electrothermal chemical guns
采用有限差分法进行数值求解，并编制了较为通用的仿真软件，用于模拟诸如由电热化学炮发射的高超声速穿甲弹弹翼前缘的瞬时热效应。 - Numerical results are in good agreement with some data and the method and procedure presented in this paper are verified . and then the wing ? flutter characters of a missile wing are numerical simulated with the examples of a missile wing
以某导弹翼面为算例，对弹翼的亚、跨、超音速的颤振临界速度进行了数值计算，部分计算结果与风洞计算结果相比较，一致性很好。