Experimental study of vortex formation in pulsating jet flow by time-resolved particle image velocimetry

We experimentally investigate the pulsating circular jet flow at moderate Reynolds numbers. By applying time-resolved particle image velocimetry in the axial-radial plane, we measure the near-field velocity fields with the jet source temporally modulated by sinusoidal pulsations. As a baseline, the steady jet flow with the same mean Reynolds number is tested. The direct comparisons of the mean and fluctuating velocity fields show that the whole potential core as well as the axisymmetric shear layer is modulated by the pulsation effect. Meanwhile, larger-scale vortices are formed in the shear layer with phase correlation of the pulsation cycle. As a result, the pulsation increases the turbulent mixing in the latter half of the potential core, and it extends the fluid entrainment further in the radial direction. The increased fluid entrainment of the ambient quiescent fluid is clearly identified by the attracting Lagrangian coherent structures as the bounds of the growing vortices within the shear layer. By analyzing the dynamic modes, we find that the low-frequency off-the-axis helical structures, which are dominant in the steady jet flow, are inhibited. The axisymmetric jet column mode and its harmonics along the axis are strengthened by the pulsation effect. Furthermore, the vortex formation mainly takes place particularly in the deceleration phase, whereas a shock-like wave front is formed during the acceleration, indicating the distinct roles of the pulsation phases in the jet instability. Published under an exclusive license by AIP Publishing.

Automated summary

We experimentally investigate the pulsating circular jet flow at moderate Reynolds numbers using time-resolved particle image velocimetry. The study shows that the pulsation effect modulates the entire potential core and the axisymmetric shear layer, forming larger-scale vortices with phase correlation. The pulsation increases turbulent mixing and extends fluid entrainment in the radial direction. Analysis of the dynamic modes reveals inhibition of low-frequency off-the-axis helical structures and strengthening of the axisymmetric jet column mode. Vortex formation mainly occurs during the deceleration phase, while a shock-like wave front is formed during acceleration.