Acoustic liners, passive devices to mitigate engine noise, operate under high-speed grazing flow and grazing acoustic waves. To investigate the complex physics governing this interaction, high-fidelity numerical simulations of a spatially evolving turbulent boundary layer grazing a multi-orifice acoustic liner at a bulk Mach number of 0.32 are performed. The simulations replicate conditions from a reference experiment. Grazing tonal plane acoustic waves with amplitudes of 130 dB and 145 dB and propagating in the same direction and the direction opposite to the mean flow are analyzed. The results show that the boundary layer displacement thickness doubles in the presence of the liner and its growth rate is affected by the amplitude and propagation direction of the acoustic wave. The acoustic liner also promotes the formation of an outer hump in both the logarithmic region of the streamwise and wall-normal velocity variance, with these effects becoming more pronounced under acoustic forcing. Furthermore, impedance estimation, using Dean’s method, reveals that near-wall flow modifications, quantified through the displacement thickness, influence the local value of the computed impedance.

ON THE INTERACTION OF GRAZING ACOUSTIC WAVES AND TURBULENT BOUNDARY LAYER OVER ACOUSTIC LINERS / Paduano, Angelo; Scarano, Francesco; Casalino, Damiano; Cordioli, Julio; Avallone, Francesco. - (In corso di stampa). ( Forum Acusticum Euronoise 2025. 11th Convention of the European Acoustics Association Malaga (ESP) 23-26 June 2025).

ON THE INTERACTION OF GRAZING ACOUSTIC WAVES AND TURBULENT BOUNDARY LAYER OVER ACOUSTIC LINERS

Paduano, Angelo;Scarano, Francesco;Casalino, Damiano;Avallone, Francesco
In corso di stampa

Abstract

Acoustic liners, passive devices to mitigate engine noise, operate under high-speed grazing flow and grazing acoustic waves. To investigate the complex physics governing this interaction, high-fidelity numerical simulations of a spatially evolving turbulent boundary layer grazing a multi-orifice acoustic liner at a bulk Mach number of 0.32 are performed. The simulations replicate conditions from a reference experiment. Grazing tonal plane acoustic waves with amplitudes of 130 dB and 145 dB and propagating in the same direction and the direction opposite to the mean flow are analyzed. The results show that the boundary layer displacement thickness doubles in the presence of the liner and its growth rate is affected by the amplitude and propagation direction of the acoustic wave. The acoustic liner also promotes the formation of an outer hump in both the logarithmic region of the streamwise and wall-normal velocity variance, with these effects becoming more pronounced under acoustic forcing. Furthermore, impedance estimation, using Dean’s method, reveals that near-wall flow modifications, quantified through the displacement thickness, influence the local value of the computed impedance.
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Utilizza questo identificativo per citare o creare un link a questo documento: https://hdl.handle.net/11583/3001533