Perturbed convective wave equation for low-to-medium Mach number subsonic flows

Schoder S, Mohamadi Bagheri E, Bogey C, Bailly C (2026)


Publication Type: Journal article

Publication year: 2026

Journal

Book Volume: 623

Article Number: 119549

DOI: 10.1016/j.jsv.2025.119549

Abstract

A generalization of the perturbed convective wave equation is proposed. It allows extracting the acoustic field and the vortical dynamics from a compressible high-fidelity flow simulation. The wave equation computes the acoustic velocity potential, with a source term based on a source potential. This source potential describes the pressure dynamics of vortices and is identical to the incompressible pressure for incompressible-modeled flows. The application to an isothermal, subsonic two-dimensional mixing layer sound generation problem validates the wave equation. The results of the acoustic far-field pressure are comparable to the direct numerical reference solution, deviating less than 1.8dB.

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APA:

Schoder, S., Mohamadi Bagheri, E., Bogey, C., & Bailly, C. (2026). Perturbed convective wave equation for low-to-medium Mach number subsonic flows. Journal of Sound and Vibration, 623. https://doi.org/10.1016/j.jsv.2025.119549

MLA:

Schoder, S., et al. "Perturbed convective wave equation for low-to-medium Mach number subsonic flows." Journal of Sound and Vibration 623 (2026).

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