Dual synthetic jets are formed by the downstream merging of two synthetic jets with a phase difference of 180°, featuring stronger momentum flux, greater penetration depth, and lower operating noise. This technology has broad application prospects in the field of flow control. This study measured the instantaneous flow fields of dual synthetic jets with an aspect ratio R_AR = 10 at operating frequencies f_A = 650, 850, 1050, and 1250 Hz by high-frequency particle image velocimetry. Coherent structures in the phase-averaged and time-averaged flow fields were analysed based on the velocity triple decomposition method and four-quadrant rule, and the entrainment capacity of the dual synthetic jets was quantitatively evaluated through mass flow rate and momentum flux. The results show that the self-support phenomenon accelerates the curvature change of the vortex ring, inhibiting the formation of inner vortices while pulling the entire vortex ring. These causes the primary vortex to deform and split off to form a secondary vortex, and promotes the transformation of minor-axis plane vorticity into the major-axis plane, leading to faster loss of coherence and collapse of the primary vortex. The time-averaged flow fields at f_A = 650 and 850 Hz exhibit a high degree of similarity, with the turbulent kinetic energy being relatively low and distributed over a large range. The periodic kinetic energy plays a dominant role in the flow field, and is mainly concentrated near the orifices. As the operating frequency increases, primary vortices are more susceptible to collapse, leading to a rapid loss of coherence. The turbulent kinetic energy caused by vortices breaking and merging becomes dominant in the flow field (f_A = 1050 and 1250 Hz), and the periodic kinetic energy is mainly concentrated in the region where primary vortices are formed. The entrainment capacity of dual synthetic jets is not solely determined by the jet Reynolds number (Re_j) or the Strouhal number (St_j), but is also closely related to the pattern of vortex evolution. The generation and development of secondary vortices can enhance the entrainment capacity, allowing the jet to maintain a high mass flow rate and momentum flux even at lower Re_j. This process is regulated by the operating frequency, which alters the evolution pattern of the primary vortex and thereby changes the streamwise evolution of the mass flow rate and the momentum flux. This study can provide a reference for the parameter optimization and engineering application of the dual synthetic jet actuator.

S-bend inlet leads to obvious flow separation and apparent total pressure distortion in unmanned aerial vehicle. To solve this problems, an active flow control method based on dual synthetic jets was proposed accordingly. The numerical simulation model of S-bend inlet with dual synthetic jets was established. The results show that dual synthetic jets can effectively suppress the boundary layer flow separation near the separation point of S-bend inlet through "blowing" and "suctioning" in the whole jet cycle, and effectively improve the total pressure recovery coefficient. The effects of different jet angles, jet peak velocities and jet frequencies on the flow field control characteristics of S-bend inlet were studied. The results shows that the smaller the angle between the dual synthetic jet and the main stream is, the better the flow separation control effect will be. The larger jet peak velocity will form a "blocking" effect on the main stream, resulting in a decrease in control effect. The closer the jet frequency is to the characteristic frequency of the flow field, the more obvious the control effect will be.

Aiming at the dynamic stall problem that restricts the improvement of aircraft maneuver-ability, a new dynamic stall control method based on leading-edge Dual Synthetic Jets (DSJ) is proposed in this paper. The aerodynamic control characteristics and flow field evolution process of steady jet, Synthetic Jet (SJ) and DSJ in dynamic stall flow field are analyzed in detail, and the corresponding control mechanism is revealed. The strong ‘‘wall attachment effect” and ‘‘quasi-steady” characteristics of DSJ are found. The results show that the leading-edge jet technology can improve the dynamic stall flow field environment. For the whole pitching process, the average lift coefficients of steady jet, SJ and DSJ increased by 3.65%, 10.51% and 14.62% respectively, and the average drag coefficients decreased by 9.58%, 29.9% and 32.0% respectively. In the downward phase, the average lift coefficient increased by 16.31%, 26.72% and 35.88% respectively, and the average drag coefficient decreased by 26.21%, 50.46% and 54.28% respectively. Due to its strong ‘‘wall attachment effect” and ‘‘quasi-steady” characteristics, DSJ exhibits optimal control effect, showing its application potential in dynamic stall control.

Even though the dual synthetic jet, a novel active flow control method with simple configuration and rapid response, does not suffer from the diaphragm failure problem common for regular synthetic jets, its performance is prone to be affected by the geometry of the jet orifice. This paper systematically studies the performance of 25 groups of dual synthetic jet actuators with different rectangular jet orifices using Particle Image Velocimetry (PIV) and numerical simulations. Specifically, the relationship between flow structures and the frequency characteristics at the jet orifice is obtained by PIV. The effects of the jet orifice's geometry on the Helmholtz resonance frequency of the actuator cavity are analyzed, yielding the optimal R_AR-R_DLR relationship. Numerical simulations are used to explore the influence of the jet orifice’s geometry on the jet velocity distribution and shaft-switching phenomenon. The results show that rectangular jet orifices with small aspect ratios produce more concentrated jet velocity with higher peak magnitude. In contrast, the velocity magnitude at rectangular jet orifices with large aspect ratios is lower; a single jet can be deflected easily by the pressure difference, but the energy exchange with the ambient fluid is more remarkable.