A Space-Time Galerkin Boundary Element Method for Aeroacoustic Scattering

TL;DR

This paper introduces a robust space-time Galerkin boundary element method for simulating aeroacoustic scattering, capable of efficiently handling complex, transient noise sources with validated accuracy against analytical solutions and experimental data.

Contribution

The paper presents a novel, stable Galerkin boundary element method with an efficient quadrature technique for aeroacoustic scattering prediction.

Findings

Excellent agreement with analytical solutions for validation cases.

Accurate predictions of scattering and shielding for complex geometries.

Good correlation with experimental measurements in practical scenarios.

Abstract

Acoustic scattering by vehicle surfaces can have significant effects on overall noise levels. In this paper, we present a space-time Galerkin time-domain boundary element method (TDBEM) that offers several distinct advantages over contemporary scattering methods for prediction of acoustic scattering and shielding of complex aeroacoustic sources such as propellers and rotors. The time-domain approach allows efficient simulation of transient, rotating, and broadband noise sources, while the Galerkin formulation is robust and unconditionally stable without any tuned numerical parameters. The main challenge of the Galerkin approach, namely the numerically difficult double space-time integration, is resolved through an efficient decomposition-based quadrature procedure. We present three cases with analytical solutions to validate the method and study its numerical properties, demonstrating excellent agreement for scattering and shielding by a variety of different geometries. We then apply the TDBEM to a trailing edge-mounted propeller case, comparing the numerical predictions with experimental measurements. The results demonstrate good agreement between predicted and measured scattering and shielding in a practical application case.