推进技术 ›› 1988, Vol. 9 ›› Issue (5): 28-33.

• • 上一篇    下一篇

液体火箭发动机燃烧过程分析

阳波,庄逢辰   

  • 发布日期:2021-08-15

COMBUSTION PROCESS ANALYSIS IN A LIQUID ROCKET ENGINE

  • Published:2021-08-15

摘要: 本文应用一维多流管耦合模型分析了液体远地点火箭发动机中的燃烧、流动过程及各因素对燃烧效率的影响.

关键词: 液体火箭发动机;燃烧;远地点发动机

Abstract: The one-dimensional coupled stream tube model is presented and used for analysis of combustion and flow processes in liquid rocket engine at apogee. The effects of various factors on combustion efficiency are also analyzed.

Key words: Liquid rocket engine;Combustion;Apogee engine