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Near-wall aerodynamic response of an acoustic liner to harmonic excitation with grazing flow
The near-orifice aerodynamic response of a single degree of freedom acoustic liner to tonal and multi-tonal excitation with grazing flow was experimentally studied. A high-magnification PIV setup was designed to provide dense 2D velocity field measurements above an orifice of the liner. The resonato...
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Published in: | Experiments in fluids 2019-09, Vol.60 (9), p.1-18, Article 144 |
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description | The near-orifice aerodynamic response of a single degree of freedom acoustic liner to tonal and multi-tonal excitation with grazing flow was experimentally studied. A high-magnification PIV setup was designed to provide dense 2D velocity field measurements above an orifice of the liner. The resonator near-orifice velocity dynamics near and far from resonance were shown to be significantly different, with dynamic velocity scales well captured by a lumped-element model that was also satisfactorily applied to multi-tonal forcing cases. The effects of varying the forcing acoustic sound pressure level and the tangential flow velocity scale (the friction velocity) were investigated. It was observed that a “rough-wall” analogy was not suited to account for the induced mean aerodynamic effects, but that, under certain conditions, a “transpiration wall” analogy may be of interest.
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doi_str_mv | 10.1007/s00348-019-2791-5 |
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subjects | Acoustic liners Acoustics Aerodynamics Engineering Engineering Fluid Dynamics Engineering Thermodynamics Flow velocity Fluid- and Aerodynamics Grazing flow Harmonic excitation Heat and Mass Transfer Orifices Research Article Sound pressure Transpiration Velocity distribution |
title | Near-wall aerodynamic response of an acoustic liner to harmonic excitation with grazing flow |
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