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THE EFFECT OF AUXILIARY FUEL IN THE CO-FLOWING AIR STREAM ON THE FLOW STRUCTURE AND BLOWOUT LIMITS OF DIFFUSION FLAMES

机译:辅助燃料在扩散火焰流动结构上的辅助燃料对流动结构和井喷限值的影响

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The paper describes the results of an investigation on the effect of an auxiliary fuel in the co-flowing air stream on the flow structure and blowout Emits of jet diffusion flames using nozzles of different geometries. Experiments were conducted with methane as the jet fuel. The auxiliary fuel in the co-flowing air stream for she majority of the tests was also methane. The flow structure of ignited jets issuing into a co-flowing stream of very lean air and methane mixtures was experimentally studied using a laser Doppler velocimeter. These tests were conducted with circular and elliptic jets of aspect ratios of 1.38 and 1.60. The diameter of the circular nozzle was 4.6 mm and the elliptic nozzles had approximately the same exit area as that of the circular nozzle. The time-averaged velocity and r.m.s value of the velocity fluctuation in the streamwise direction were measured for a co-flowing stream velocity of 1.21 m/s which corresponds to the blowout of attached flames in an &only co-flowing stream. On the basis of these measurements, attempts were made to explain the effect of nozzle geometry on the flame blowout limits.
机译:本文描述了一种辅助燃料的共同流动的空气流中在流结构和使用井喷不同几何形状喷嘴喷射扩散火焰的发射的影响的调查结果。实验用甲烷作为喷气燃料进行。因为她大部分测试的共同流动的空气流中的辅助燃料也是甲烷。点燃射流发放到非常稀薄的空气和甲烷的混合物的共流动流的流动结构使用激光多普勒测速仪进行实验研究。这些测试用的1.38和1.60的长宽比的圆形和椭圆射流进行。圆形喷嘴的直径为4.6毫米,喷嘴椭圆具有大致相同的出射面为圆形喷嘴的。的时间平均的速度和在所述流动方向的速度变动的r.m.s值分别为1.21米/秒的共流流速度下测量,其对应于附着火焰的吹出在与仅共同流入流。这些测量的基础上,尝试作了解释喷嘴几何形状上的火焰喷出的限制的影响。

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