The nonlinear highfrequency combustion instability process in the liquid rocket engine is simulated with the method of nonlinear dynamics.
采用非线性动力学方法对液体火箭发动机非线性高频燃烧不稳定工作过程进行了研究。
2
There is limited evidence that the mechanism for highfrequency combustion instability lies in the vaporization and combustion processes.
有限的证据表明，高频燃烧不稳定性机理取决于汽化和燃烧过程。
3
This paper presents computation and analysis of tangential mode of highfrequency combustion instability in FY-20 liquid propellant rocket engine by means of the annular instability model.