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SUBADIABATIC AND SUPERADIABATIC PERFORMANCE OF A TWO-SECTION POROUS BURNER

机译:两部分多孔燃烧器的亚绝热和超绝热性能

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Flames may be stabilized in porous media at velocities either above or below the laminar flame speed. These two regimes are often called superadiabatic and subadiabatic, respectively. In this paper, several burners are investigated experimentally at both superadiabatic and subadiabatic conditions. The upper and lower velocity limits of stable combustion are reported. For equivalence ratios of 0.70 and below, both sub- and superadiabatic performance was seen. For both sub- and superadiabatic performance, the flame was stabilized at or near the interface between the upstream and downstream sections of porous media. The lower velocity limit for superadiabatic performance was extinction of the flame. The upper limit for superadiabatic performance was blowoff, which occurred for all burners at a flow velocity several times the adiabatic laminar flame speed, a phenomenon which is attributed to heat recirculation within the porous media. For equivalence ratios above 0.70, only subadiabatic performance was observed. The lower velocity limit occurred when the flame reached extinction. The upper velocity limit occurred when heat recirculation enhanced the laminar flame speed to a point at which the flame front propagated through the upstream section of porous media and flashed back upstream of the burner. Both the upper and lower velocity limits minimized at or near an equivalence ratio of 1.1. For equivalence ratios between 1.3 and 1.7 and flow velocities between 4 and 9 cm/s, oscillations of the flame front within the downstream section of porous media were observed.
机译:火焰可以在多孔介质中以高于或低于层流火焰速度的速度稳定。这两种制度通常分别称为超级绝热和亚绝热。本文在超级绝热和亚绝热条件下对几种燃烧器进行了实验研究。报告了稳定燃烧的速度上限和下限。当等效比为0.70或更低时,可以看到亚绝热和超级绝热性能。对于亚绝热性能和超绝热性能,火焰稳定在多孔介质上游和下游部分之间的界面处或附近。超绝热性能的下限速度是火焰的熄灭。超级绝热性能的上限是吹气现象,该现象在所有燃烧器中均以绝热层流火焰速度几倍的流速发生,这种现象归因于多孔介质内的热循环。当等效比大于0.70时,仅观察到绝热性能。当火焰熄灭时出现下限速度。当热量再循环将层流火焰速度提高到火焰前沿传播通过多孔介质的上游部分并闪回到燃烧器上游时,便出现了速度上限。当等于或接近1.1时,速度上限和下限均最小化。对于当量比在1.3和1.7之间以及流速在4和9 cm / s之间的情况,观察到多孔介质下游区域内火焰前锋的振荡。

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