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      Aeroacoustic Source Potential Based on Poisson’s Equation

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          Abstract

          Poisson’s equation is an important equation to postprocess the aerodynamic fields into linearized momentum modes and was recently found to be important for the computation of an isotropic pressure-like source for scalar aeroacoustic wave models, like the aeroacoustic wave equation based on Pierce’s operator (AWE-PO). Mathematically viable boundary conditions of the Poisson equation, which computes the AWE-PO source, are investigated. For the different source fields, the wave propagation is computed using the AWE-PO, and the details of the sound prediction results are compared to a reference direct numerical simulation of a mixing layer. The different boundary conditions of the Poisson equation were found to have a minor influence on the overall sound prediction characteristics of the AWE-PO equation. The AWE-PO is reformulated into a simplified version of the Phillips’s equation, which mitigates the intermediate step of computing an isotropic source potential. By doing so, a previously obtained interference radiation valley in the radiated acoustic intensity of the AWE-PO results is attributed to a missing shear-noise source term.

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                Author and article information

                Contributors
                Journal
                aiaaj
                AIAA Journal
                AIAA Journal
                American Institute of Aeronautics and Astronautics
                1533-385X
                26 April 2024
                July 2024
                : 62
                : 7
                : 2772-2782
                Affiliations
                Graz University of Technology , 8010 Graz, Austria
                Friedrich-Alexander-Universität , 91058 Erlangen, Germany
                Hong Kong University of Science and Technology , Clear Water Bay, New Territories, Hong Kong SAR, People’s Republic of China
                Author notes
                [*]

                Assistant Professor, Institute of Fundamentals and Theory in Electrical Engineering (IGTE), Inffeldgasse 18; also Visiting Scholar at Institute of Fluid Mechanics (LSTM), Friedrich-Alexander-Universität, 91058 Erlangen, Germany; stefan.schoder@ 123456tugraz.at . Member AIAA (Corresponding Author).

                [†]

                Doctoral Candidate, Institute of Fluid Mechanics (LSTM).

                [‡]

                Postdoctoral Fellow, Department of Mechanical and Aerospace Engineering.

                Author information
                https://orcid.org/0000-0002-2148-6703
                https://orcid.org/0000-0001-6214-776X
                Article
                J063792 J063792
                10.2514/1.J063792
                b9f5a096-72b6-4f38-9c45-c1dd21c8d226
                Copyright © 2024 by the authors. All rights reserved. All requests for copying and permission to reprint should be submitted to CCC at www.copyright.com; employ the eISSN 1533-385X to initiate your request. See also AIAA Rights and Permissions www.aiaa.org/randp.
                History
                : 27 November 2023
                : 18 February 2024
                : 22 March 2024
                Page count
                Figures: 13, Tables: 2
                Funding
                Funded by: Hong Kong Research Grants Council
                Award ID: 16204721
                Funded by: Hong Kong Innovation and Technology Commission
                Award ID: ITS/301/20FP
                Categories
                p3421, General Physics
                p3317, Mathematical Analysis
                p2263, Fluid Dynamics
                p3282, Computational Fluid Dynamics
                p1805, Aeroacoustics
                p2228, Aerospace Sciences
                p2073, Aeronautics
                p2187, Computing, Information, and Communication
                p16679, Computing and Informatics
                Regular Articles

                Engineering,Physics,Mechanical engineering,Space Physics
                Mathematical Analysis,Computing and Informatics,Aeroacoustics,Computational Fluid Dynamics

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