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Blow-out limits of nonpremixed turbulent jet flames in a cross flow at atmospheric and sub-atmospheric pressures

机译:大气压和低于大气压的错流中非预混湍流射流的爆破极限

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摘要

The blow-out limits of nonpremixed turbulent jet flames in cross flows were studied, especially concerning the effect of ambient pressure, by conducting experiments at atmospheric and sub-atmospheric pressures. The combined effects of air flow and pressure were investigated by a series of experiments conducted in an especially built wind tunnel in Lhasa, a city on the Tibetan plateau where the altitude is 3650 m and the atmospheric pressure condition is naturally low (64 kPa). These results were compared with results obtained from a wind tunnel at standard atmospheric pressure (100 kPa) in Hefei city (altitude 50 m). The size of the fuel nozzles used in the experiments ranged from 3 to 8 mm in diameter and propane was used as the fuel. It was found that the blow-out limit of the air speed of the cross flow first increased (“cross flow dominant” regime) and then decreased (“fuel jet dominant” regime) as the fuel jet velocity increased in both pressures; however, the blow-out limit of the air speed of the cross flow was much lower at sub-atmospheric pressure than that at standard atmospheric pressure whereas the domain of the blow-out limit curve (in a plot of the air speed of the cross flow versus the fuel jet velocity) shrank as the pressure decreased. A theoretical model was developed to characterize the blow-out limit of nonpremixed jet flames in a cross flow based on a Damköhler number, defined as the ratio between the mixing time and the characteristic reaction time. A satisfactory correlation was obtained at relative strong cross flow conditions (“cross flow dominant” regime) that included the effects of the air speed of the cross flow, fuel jet velocity, nozzle diameter and pressure.
机译:通过在大气压和低于大气压下进行实验,研究了横流中非预混湍流喷射火焰的爆破极限,特别是关于环境压力的影响。气流和压力的综合影响是通过在西藏高原海拔3650 m,气压自然很低(64 kPa)的拉萨市一座特别建造的风洞中进行的一系列实验研究的。将这些结果与合肥市(海拔50 m)在标准大气压(100 kPa)下的风洞获得的结果进行了比较。实验中使用的燃料喷嘴的尺寸为直径3至8毫米,丙烷用作燃料。发现在两个压力下,横流空气速度的喷出极限首先增加(“横流主导”状态),然后降低(“燃料射流主导”状态)。但是,在低于大气压的情况下,横流气流速度的吹出极限比在标准大气压下要低得多,而吹出极限曲线的范围(在横流空气速度图中流量与燃油喷射速度的关系)随着压力的降低而缩小。建立了一个理论模型,以基于Damköhler数来表征错流中非预混射流火焰的吹出极限,该值定义为混合时间与特征反应时间之间的比值。在相对强的错流条件下(“错流主导”状态)获得了令人满意的相关性,其中包括错流的空气速度,燃料喷射速度,喷嘴直径和压力的影响。

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