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Flow Visualization and Characteristics of a Coaxial Jet with a Tabbed Annular Nozzle

机译:带环形环形喷嘴的同轴射流的流动可视化和特性

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摘要

Flow visualization and measurements of mean and fluctuating velocities were performed on a coaxial jet with a velocity ratio of 0.6 at a Reynolds number of 3 000 in an open water tank using hot-film anemometry, particle image velocimetry (2D and stereoscopic PIV) and laser-induced fluorescence (LIF). Axisymmetric and streamwise vortical structures were revealed in the near-field of the coaxial jet. The annular nozzle has six vortex generators in order to enhance the streamwise vortices generated in the mixing layer. Furthermore, the annular jet was excited by a shaker in order to enhance the axisymmetric vortices. For the tabbed coaxial jet, jet spreading downstream was greater than for the jet without tabs. The cause of the entrainment increment is the development of axisymmetric and streamwise vortex structures. In the case of excited jets, significant axisymmetric and streamwise vortical structures develop, and the jet width expands from the exit nozzle. Consequently, the flow rate of the excited jet with tabs is larger than that of the unexcited jet without tabs.
机译:使用热膜风速仪,颗粒图像测速仪(2D和立体PIV)和激光在开放水箱中的雷诺数为3000的同轴射流上以0.6的速度比对同轴射流进行流动可视化以及平均速度和脉动速度的测量-诱导的荧光(LIF)。在同轴射流的近场中揭示了轴对称和沿流方向的涡旋结构。环形喷嘴具有六个涡流发生器,以增强在混合层中产生的沿流方向的涡流。此外,环形射流被振动器激发,以增强轴对称涡旋。对于带凸片的同轴射流,向下游扩展的射流比没有凸片的射流大。夹带增加的原因是轴对称涡流结构的发展。在激发射流的情况下,会形成明显的轴对称和沿流的涡旋结构,射流宽度会从出口喷嘴扩展。因此,带有翼片的激发射流的流速比没有翼片的未激发射流的流速大。

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