Experimental analysis reveals that synthetic jets reduce drag and enhance flow control in turbulent flows, suggesting improved efficiency for underwater vehicles.
To reveal the regulatory mechanisms of synthetic jets on coherent structures in a flat-plate turbulent boundary layer at a low friction Reynolds number of 489, single-slot and double-slot synthetic jet configurations were designed. Particle image velocimetry measurements were coupled with three analytical methods, including two-point correlation, space-time correlation, and linear stochastic estimation, to systematically investigate the streamwise evolution of coherent structures and associated drag reduction influences. Experimental results indicate that the double-slot jets achieve an average drag reduction rate of 21.76%, obviously outperforming the single-slot jets, which attain 14.45%. The peak drag reduction rate reaches 25.60% for the double-slot configuration, compared to 20.18% for the single-slot counterpart, while showing weaker streamwise attenuation in control efficacy. Synthetic jets suppress turbulent bursting and interlayer momentum exchange by lifting near-wall low-momentum fluids, compressing the spatiotemporal scales of coherent structures, reducing their migration velocity, and augmenting sweep velocity. The secondary disturbance of the double-slot jets extends the streamwise control range and enhances the disruption of large-scale hairpin vortex packets. This study offers robust experimental and theoretical support for the development of low-power-consumption drag reduction technologies for underwater vehicles.
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Li et al. (2026) studied this question.
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