The Effects of Nozzle Orientation on Mixing Characteristics of Elliptic Twin Free Jets

Ella M. Morris, Neelakash Biswas, Seyed Sobhan Aleyasin, M. Tachie
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引用次数: 2

Abstract

The effects of nozzle orientation on the mixing and turbulent characteristics of elliptical free twin jets were studied experimentally. The experiments were conducted using modified contoured nozzles with a sharp linear contraction. The centers of the nozzle pair had a separation ratio of 5.5. Four nozzle configurations were tested, one twin jet orientated along the minor plane (Twin_Minor), one twin jet orientated along the major plane (Twin_Major), one single jet orientated along the minor plane (Single_Minor) and one single jet orientated along the major plane (Single_Major). In each case, the Reynolds number based on the maximum jet velocity and the equivalent diameter was 10,000. A planar particle image velocimetry system was used to measure the velocity field in the jet symmetry plane. It was observed that the velocity decay rate is not sensitive to nozzle orientation. However, close to the jet exit the spread rate was highest in the minor plane. In addition, contour plots of Reynolds shear stress and turbulence intensities revealed significant differences between the minor and major plane. Velocity profiles showed little variation close to the jet exit, while further downstream the variations between the velocity profiles were more pronounced between the major and minor planes.
喷嘴取向对椭圆双自由射流混合特性的影响
实验研究了喷嘴取向对椭圆自由双射流混合和湍流特性的影响。实验采用带直线急剧收缩的改进型喷嘴进行。喷嘴对中心的分离比为5.5。测试了四种喷嘴配置,一种是沿小平面定向的双射流(Twin_Minor),一种是沿大平面定向的双射流(Twin_Major),一种是沿小平面定向的单射流(Single_Minor),一种是沿大平面定向的单射流(Single_Major)。在每种情况下,基于最大射流速度和等效直径的雷诺数为10,000。采用平面粒子图像测速系统对射流对称平面内的速度场进行了测量。结果表明,射流速度衰减率对喷嘴取向不敏感。而靠近喷气出口的小平面传播率最高。此外,雷诺数剪应力和湍流强度等值线图也显示出主、小平面之间存在显著差异。射流出口附近的速度分布变化不大,而在较下游的主要和次要平面之间的速度分布变化更为明显。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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