1) inner launch-trajectory equations
内弹道方程组
1.
The inner launch-trajectory equations and vapor-discharge equation for deck-landing aircrafts were established.
建立了舰载机弹射内弹道方程组和蒸汽流量方程,根据内弹道设计指标要求和飞机参数对弹射过程进行了仿真计算。
2) interior ballistic equations
内弹道方程
1.
Aimed at the complexity and real law of loads on gun tube in the process of projectile lanuch,based on the interior ballistic equations,taken account of the flexible effect of gun tube,the dynamic coupling equations that describe the vibration response law were established.
针对火炮发射过程中身管受载的复杂性,以内弹道方程为基础,考虑发射过程中身管受载的实际规律,计及身管的柔性效应,建立描述身管振动响应规律的动力学方程组。
3) trajectory equations
弹道方程组
1.
This paper presents an algorithm for finding projectile flight time with ensured acccuracy by solving the trajectory equations with unknown angle of departure only one time.
提出一种在保证一定计算精度的前提下，只解一次弹道方程组就可求得未知射角情况下目标点相应弹丸飞行时间的算法，而不需要在先求得准确射角后再解一次弹道方程组求解。
4) equations of point-mass trajectory
质点弹道方程组
5) ballistic differential equation
弹道微分方程组
6) calculate ballistic trajectory equations
解弹道方程组
补充资料：弹道(见弹道学)
弹道(见弹道学)
trajectory
dQfldQO弹道(t rajectory)见弹道学。
说明：补充资料仅用于学习参考，请勿用于其它任何用途。
参考词条