圆形射流近场的三维空间

B. Ganapathisubramani, Arnauld Loyer, E. Longmire, I. Marusic
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引用次数: 2

摘要

利用立体PIV技术研究了一个圆形空气射流(Re = 16000),了解了发展中的剪切层中所有三个速度分量的特征,并研究了三维空间随轴向距离的演变。脉冲激光片被排列以照亮射流的中心线平面。对立体PIV设置进行了适当的校准,以将所得像素位移转换为轴向、径向和方位角速度分量。Y/D ~ 0.5下游剪切层的方位速度均方根值约为0.1Vo。这比以前的研究报告要早得多。个别场显示涡旋核和编织都是三维的。然而,最初的方位角扰动通常与第一个形成的旋涡环上游的紧张区域有关。
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THREE DIMENSIONALITY IN THE NEAR FIELD OF A ROUND JET
A round air jet (Re = 16000) was studied using Stereo PIV techniques to understand the characteristics of all three velocity components in the developing shear layer and to study the evolution of three dimensionality with increasing axial distance. Pulsed laser sheets were aligned to illuminate the centerline plane of the jet. The stereo PIV setup was suitably calibrated to translate the resulting pixel displacements into axial, radial, and azimuthal velocity components. The RMS of the azimuthal velocity is of the order of 0.1Vo in the shear layer downstream of Y/D ~ 0.5. This is significantly earlier than reported in previous studies. Individual fields show that both vortex cores and braids are three dimensional. However, the initial azimuthal perturbations typically were associated with straining regions immediately upstream of the first vortex ring that formed.
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