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- W2017990062 abstract "An experimental investigation was performed to study the three-dimensional flow structures and interactions of a finite-span synthetic jet with the flow over a finite and swept back wing (cross-sectional profile of the NACA 4421, AR=4, sweep angle of 30 deg), at a Reynolds number of 10 5 and zero angle of attack. Two momentum coefficients were considered, corresponding to two blowing ratios of 0.8 and 1.2. Stereoscopic PIV data was collected around the center jet in the mid-span section. The effect of the momentum coefficient (or blowing ratio) was analyzed based on the three-dimensional flow field using time-averaged and phase-averaged statistics. The study showed that, similar to the interaction of a synthetic jet with the flow over an unswept wing, the flow field in the vicinity of the synthetic-jet orifice becomes highly three-dimensional and is governed by the superposition of two kinds of flow structures: (1) streamwise structures that are associated with the finite span of the jet (edge vortices), and (2) spanwise flow structures that are generated along the orifice due to the vortex pairs that are formed by the synthetic jet. Nevertheless, over a swept wing these three-dimensional flow structures evolve almost immediately downstream to the synthetic-jet orifice and evolve into a very complex 3-D flow field." @default.
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- W2017990062 date "2010-11-01" @default.
- W2017990062 modified "2023-09-26" @default.
- W2017990062 title "Interaction of a Finite-span Synthetic-jet and Cross-flow over a Swept Wing" @default.
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