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(dòng)機(jī)燃燒室一維兩相常滯后流動(dòng)。
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(shí)時(shí)脈沖取樣器用于測(cè)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(jì)算方法可用于小型固體火箭發(fā)動(dòng)機(jī)的工程計(jì)算，有一定的應(yīng)用價(jià)值。