Noise Scattering by Regularized Boundary Elements and Ffowcs–Williams and Hawkings Method

In this paper, the authors present a method for computing noise scattering against solid bodies. The method is based on coupling the Ffowcs–Williams and Hawkings (FW-H) method with a regularized boundary element method (BEM). The benefit of the chosen approach is that the computation of the noise sources, which is typically done with high-fidelity computational fluid dynamics/computational aeroacoustics, is decoupled from the noise-scattering problem. This makes it possible to consider several different configurations of a scattering body using a single simulation of the noise sources. In the paper, the authors provide a detailed description of the two methods (FW-H and BEM) as well as how they are coupled. They also demonstrate the accuracy of the chosen approach by applying it to a set of test cases with analytical solutions. Finally, they use the coupled FW-H/BEM approach to compute the acoustic loads on the rear parts of two business jet fuselages and compare the numerical results to experimental data obtained by The German Aerospace Center (DLR), German Aerospace Center in the Aeroacoustic Wind Tunnel of Braunschweig.

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Publication Details

Journal
AIAA Journal
Published
2026-01-19
DOI
https://doi.org/10.2514/1.j065985
Primary Topic
Aerodynamics and Acoustics in Jet Flows
Type
article
Field-Weighted Citation Impact
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article

Noise Scattering by Regularized Boundary Elements and Ffowcs–Williams and Hawkings Method

U. Michel, Daniel Lindblad, Maximilian Höchel, Hao Xia
AIAA Journal
Aerodynamics and Acoustics in Jet Flows
article

Noise Scattering by Regularized Boundary Elements and Ffowcs–Williams and Hawkings Method

U. Michel, Daniel Lindblad, Maximilian Höchel, Hao Xia
article en

Abstract

In this paper, the authors present a method for computing noise scattering against solid bodies. The method is based on coupling the Ffowcs–Williams and Hawkings (FW-H) method with a regularized boundary element method (BEM). The benefit of the chosen approach is that the computation of the noise sources, which is typically done with high-fidelity computational fluid dynamics/computational aeroacoustics, is decoupled from the noise-scattering problem. This makes it possible to consider several different configurations of a scattering body using a single simulation of the noise sources. In the paper, the authors provide a detailed description of the two methods (FW-H and BEM) as well as how they are coupled. They also demonstrate the accuracy of the chosen approach by applying it to a set of test cases with analytical solutions. Finally, they use the coupled FW-H/BEM approach to compute the acoustic loads on the rear parts of two business jet fuselages and compare the numerical results to experimental data obtained by The German Aerospace Center (DLR), German Aerospace Center in the Aeroacoustic Wind Tunnel of Braunschweig.

AIAA Journal
Loughborough University (GB), Gesellschaft für Fertigungstechnik und Entwicklung (DE)
Affordable and clean energy
Openalex Percentile: Top 65%
Aerodynamics and Acoustics in Jet Flows
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