Acoustic Impedance of Circular Perforates Subjected to Grazing Flow
This paper develops a semi-empirical acoustic impedance model of circular perforates under a low-Mach-number ([Formula: see text]) grazing air flow. The formulation combines a no-flow impedance, appropriate to the high–Strouhal-number ([Formula: see text]) regime, and a with-flow impedance given by the low-Strouhal-number asymptotic limit of the proposed linear theory. The model accounts for viscous losses, shear-flow effects, coupling between adjacent orifices, porous media via complex effective densities, and acoustic nonlinearities at high sound-pressure levels (SPLs). Realistic shear-layer convection is represented by an empirical phase-speed factor [Formula: see text], whose real and imaginary parts primarily affect the acoustic resistance and reactance, respectively. Validation against published experimental datasets ([Formula: see text], [Formula: see text], and [Formula: see text]) indicates that, for air-backed configurations, [Formula: see text]. with [Formula: see text], whereas for porous-backed configurations, we adopt [Formula: see text] and neglect [Formula: see text]. Overall, the model shows good agreement with experiments and robustness across representative operating conditions. As a limitation, the model does not capture certain behaviors that may arise at moderate [Formula: see text] (e.g., negative resistance and coupling between grazing flow and acoustic nonlinearity), which lie beyond the present scope.
Authors
- Thomas Humbert (ORCID: https://orcid.org/0000-0003-3783-5290)
- Long Wu (ORCID: https://orcid.org/0009-0006-8578-7755)
- Yang Meng (ORCID: https://orcid.org/0000-0001-5646-462X)
- Gwénaël Gabard
Institutions
- Le Mans Université (FR)
- University of Southampton (GB)
- Centre de Recherche en Éducation de Nantes (FR)
Publication Details
- Journal
- AIAA Journal
- Published
- 2026-02-09
- DOI
- https://doi.org/10.2514/1.j065690
- Primary Topic
- Aerodynamics and Acoustics in Jet Flows
- Type
- article
- Field-Weighted Citation Impact
- 0.00