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首页> 外文期刊>European Journal of Mechanics, B. Fluids >Experimental study of the near field and transition region of a free jet issuing from a sharp-edged elliptic orifice plate
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Experimental study of the near field and transition region of a free jet issuing from a sharp-edged elliptic orifice plate

机译:锋利的椭圆孔板产生自由射流的近场和过渡区的实验研究

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The mixing characteristics in the near field and transition region, the region of interest in most jet mixing applications, of an isothermal, incompressible, free jet of air issuing from a sharp-edged elliptic orifice plate of aspect ratio 2 into still air surroundings have been studied experimentally using hot-wire anemometry and a pitot-static tube. For comparison, some experiments were performed in round jets issuing from a sharp-edged orifice plate and from a contoured nozzle. All the test jets were unforced and the Reynolds number, based on the equivalent diameter of the sharp-edged elliptic orifice plate which was the same as the diameter of the sharp-edged round orifice plate or the contoured round nozzle, was 1.88 × 10{sup}5. The three components of the mean velocity vector, time-averaged and phase-averaged fluctuating velocity data, autocorrelation coefficients and one-dimensional spectra of the fluctuating velocities and the mean static pressure were measured. The mean streamwise vorticity, mass entrainment rates and the jet half-velocity widths have been obtained from the measured data. The results show that mixing in an elliptic jet issuing from a sharp-edged orifice plate is higher than in round jets and in elliptic jets issuing from contoured nozzles. The near field and transition region of the elliptic jet were deduced to be dominated by the axisymmetric instability mode which triggers the generation of symmetric shear layer structures. The results also show the presence of coherent structures in the near field and transition region of the jet and the effect of these coherent structures on momentum transport in the jet.
机译:从纵横比为2的尖锐椭圆形孔板向静止空气环境中喷射的等温,不可压缩的自由射流在近场和过渡区域(大多数射流混合应用中感兴趣的区域)的混合特性已得到证实使用热线风速仪和皮托管来进行实验研究。为了进行比较,在从尖锐的孔板和轮廓喷嘴发出的圆形射流中进行了一些实验。所有测试喷嘴均未受力,基于锐边椭圆形孔板的等效直径与锐边圆形孔板或轮廓形圆形喷嘴的直径相同,雷诺数为1.88×10 { sup} 5。测量了平均速度矢量,时间平均和相位平均波动速度数据,自相关系数以及波动速度和平均静压的一维频谱的三个分量。已从测量数据获得了平均流向涡度,质量夹带率和射流半速度宽度。结果表明,从锋利的孔板射出的椭圆形射流的混合比圆形射流和从轮廓状喷嘴射出的椭圆形射流的混合高。推论出椭圆射流的近场和过渡区域受轴对称失稳模式支配,从而触发了对称剪切层结构的产生。结果还表明,在射流的近场和过渡区域中存在相干结构,以及这些相干结构对射流中动量传输的影响。

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