solid-propellant motors

基本解釋

In this paper, one-dimensional two-phase constant lag flow in combustion chamber of solid propellant rocket motors is described.
本文論述了固體火箭發(fā)動機(jī)燃燒室一維兩相常滯后流動。
A real-time impulsive particle sampling technique has been discussed to measure the particulate size distribution in solid propellant rocket motors.
介紹一種實時脈沖取樣器用于測定團(tuán)體火箭燃燒室內(nèi)凝相微粒尺寸分布技術(shù)。
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.
從而表明提出的計算方法可用于小型固體火箭發(fā)動機(jī)的工程計算，有一定的應(yīng)用價值。