solid-propellant motors

基本解释

In this paper, one-dimensional two-phase constant lag flow in combustion chamber of solid propellant rocket motors is described.
本文论述了固体火箭发动机燃烧室一维两相常滞后流动。
A real-time impulsive particle sampling technique has been discussed to measure the particulate size distribution in solid propellant rocket motors.
介绍一种实时脉冲取样器用于测定团体火箭燃烧室内凝相微粒尺寸分布技术。
The results from calculation and experiments are in good agreement. It indicates that this method, is suitable for small-scale solid propellant rocket motors, and therefore of practical significance.
从而表明提出的计算方法可用于小型固体火箭发动机的工程计算，有一定的应用价值。