环形不稳定性计算模型在FY-20液体火箭发动机上的应用
APPLICATION OF ANNULAR INSTABILITY MODEL TO FY-20 LIQUID PROPELLANT ROCKET ENGINE
-
摘要: 本文用环形不稳定性计算模型计算、分析了FY-20液体火箭发动机的切向高频燃烧不稳定性。其结果与热试车结果是一致的。根据所得结果,为此发动机中安装径向隔板的必要性提供了理论依据井对稳定性不佳的液体火箭发动机提出了具体改进步骤及一些有效措施。Abstract: This paper presents computation and analysis of tangential mode of high frequency combustion instability in FY-20 liquid propellant rocket engine by means of the annular instability model. The results show that the tangential mode of high frequency unstable conbustion does not occur in the engine, that coincides with the experimental results. Concrete steps and some effective measures for improving the liquid propellant rocket engine which is weak in the tangential mode of high frequency stability are also described in the paper.
点击查看大图
计量
- 文章访问数: 1728
- HTML浏览量: 8
- PDF量: 384
- 被引次数: 0