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Stability of a Spontaneous Vortex Structure in Flame under Gas Oscillations

机译:气体振荡下火焰中自发涡旋结构的稳定性

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The stability of a spontaneous vortex structure formed during combustion of a gas injected through a round hole in a flat horizontal plate onto its lower surface was studied. The unsteady velocity, vorticity, temperature, and pressure fields in the vortex structure were studied experimentally and numerically. It is established that for Reynolds numbers Re approx = 10-75 and Rayleigh numbers Ra approx = 10~3-10~4, the vortex structure is stable against single velocity perturbations and changes under acoustic oscillations with a frequency of 100-150 Hz. Small cells whose dimensions are comparable with the flame front thickness are destroyed, and the velocity of the vortex gas flow in large cells changes with the frequency of forced oscillations. The amplitude of linear gas velocity oscillations in the vortex is larger than that of gas velocity oscillations in the burner nozzle. It is assumed that the observed increase in the amplitude of gas velocity oscillations in the vortex is due to both acceleration of the combustion products in the gravity field and their thermal expansion. The gas velocity oscillations in the vortex structure lag behind the gas flow rate oscillations by a quater of the period.
机译:研究了通过水平平板中的圆孔注入气体的自燃涡流结构的稳定性,该气体通过水平平板向其下表面喷射。实验和数值研究了涡结构中的非定常速度,涡度,温度和压力场。可以确定的是,对于雷诺数Re近似= 10-75和瑞利数Ra近似= 10〜3-10〜4,涡旋结构对于单次速度摄动和在100-150 Hz频率的声振荡下的变化是稳定的。尺寸与火焰前壁厚度相当的小单元被破坏,大单元中涡流的流动速度随强迫振荡的频率而变化。涡流中的线性气体速度振荡的幅度大于燃烧器喷嘴中的气体速度振荡的幅度。假设在涡流中观察到的气体速度振荡幅度的增加是由于燃烧产物在重力场中的加速及其热膨胀引起的。涡旋结构中的气体速度振荡滞后于该期间的四分之一的气体流速振荡。

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