2015
DOI: 10.1016/j.sna.2015.05.018
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Numerical study of nozzle design for the hybrid synthetic jet actuator

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Cited by 7 publications
(4 citation statements)
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“…Although there is no net mass transfer to ambient fluid, the device has the interesting feature of transferring a finite amount of momentum to the ambient fluid. [5,7,19,20] Based on this principle, a schematic illustration of our synthetic jet actuator design is shown in Figure 1, including the proposed structure of the DE-based synthetic jet actuator (Figure 1a), the ejection stroke ( Figure 1b), and the suction stroke ( Figure 1c). The 4 Â 4 biaxially prestretched DE membrane (VHB4910, 3M) was fixed in a 3D printed photosensitive resin frame.…”
Section: Propulsion Mechanism Of Synthetic Jet Using Dementioning
confidence: 99%
See 1 more Smart Citation
“…Although there is no net mass transfer to ambient fluid, the device has the interesting feature of transferring a finite amount of momentum to the ambient fluid. [5,7,19,20] Based on this principle, a schematic illustration of our synthetic jet actuator design is shown in Figure 1, including the proposed structure of the DE-based synthetic jet actuator (Figure 1a), the ejection stroke ( Figure 1b), and the suction stroke ( Figure 1c). The 4 Â 4 biaxially prestretched DE membrane (VHB4910, 3M) was fixed in a 3D printed photosensitive resin frame.…”
Section: Propulsion Mechanism Of Synthetic Jet Using Dementioning
confidence: 99%
“…The synthetic jet actuator proposed in this article can be described as a zero‐net‐mass‐flux actuator because the integral of the mass flow rate across the orifice over an integer number of cycles is equal to zero. Although there is no net mass transfer to ambient fluid, the device has the interesting feature of transferring a finite amount of momentum to the ambient fluid . Based on this principle, a schematic illustration of our synthetic jet actuator design is shown in Figure , including the proposed structure of the DE‐based synthetic jet actuator (Figure a), the ejection stroke (Figure b), and the suction stroke (Figure c).…”
Section: Propulsion Mechanism Of Synthetic Jet Using Dementioning
confidence: 99%
“…The integration of fluid diodes is designed to rectify oscillating air flow to suppress the backflow of hot (heated) air through the nozzle exit in the suction stroke. The volumetric efficiency is thus introduced to evaluate the rectifying effect of the proposed hybrid synthetic jet actuators on the air flow, which can be defined as [30]  = − + (10) where represents the air volume ejected out through the nozzle exit in one cycle by the actuators and denotes the air volume sucked back through the nozzle exit in one cycle.…”
Section: Calculation Of Dimensionless Parametersmentioning
confidence: 99%
“…A modification of this technique using the Coanda effect was recently reported by Song et al [24] and He et al [25]. Finally, based on the working principle of a chain of vortexes, many design variants, for example, the combination of diffuser-nozzle or fluidic diode with the synthetic jet [26] [27], batwing-junction [28], T-junction [29], internal vortex membrane [30] were successfully applied in droplet forming, pinching, circulating or simultaneously pumping and mixing. Thus, it is reasonable to assume that the synthetic jet is a potential technique for improving the pumping performance by a smart structure which can enhance counter-rotating vortexes.…”
Section: Introductionmentioning
confidence: 99%