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A new strategy towards stable and accurate boundary closures for high-order finite difference schemes

A new strategy towards stable and accurate boundary closures for high-order finite difference schemes
A new strategy towards stable and accurate boundary closures for high-order finite difference schemes

This paper presents a generalised strategy to develop linearly stable and accurate boundary closure schemes for large-stencil, high-order, finite difference systems in computational aero acoustics. The optimisation problem is formulated to maximise the global accuracy of the differencing system under a linear stability constraint evaluated by eigenvalue analysis. The strategy for constructing boundary schemes is based on an interpolation-differentiation procedure. Three sets of optimised boundary closure schemes have been presented for three widely used central schemes in computational aero acoustics. The present boundary schemes, when used together with the corresponding central scheme, are guaranteed to be linearly stable. Moreover, they are more accurate compared with the previous boundary schemes optimised for resolution.

Wu, Long
9787473b-a81a-47ce-a696-22afa8c2204b
Kim, Jae-Wook
fedabfc6-312c-40fd-b0c1-7b4a3ca80987
Wu, Long
9787473b-a81a-47ce-a696-22afa8c2204b
Kim, Jae-Wook
fedabfc6-312c-40fd-b0c1-7b4a3ca80987

Wu, Long and Kim, Jae-Wook (2024) A new strategy towards stable and accurate boundary closures for high-order finite difference schemes. In 30th AIAA/CEAS Aeroacoustics Conference (2024). (doi:10.2514/6.2024-3361).

Record type: Conference or Workshop Item (Paper)

Abstract

This paper presents a generalised strategy to develop linearly stable and accurate boundary closure schemes for large-stencil, high-order, finite difference systems in computational aero acoustics. The optimisation problem is formulated to maximise the global accuracy of the differencing system under a linear stability constraint evaluated by eigenvalue analysis. The strategy for constructing boundary schemes is based on an interpolation-differentiation procedure. Three sets of optimised boundary closure schemes have been presented for three widely used central schemes in computational aero acoustics. The present boundary schemes, when used together with the corresponding central scheme, are guaranteed to be linearly stable. Moreover, they are more accurate compared with the previous boundary schemes optimised for resolution.

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More information

e-pub ahead of print date: 30 May 2024
Published date: 4 June 2024
Additional Information: Publisher Copyright: © 2024, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.

Identifiers

Local EPrints ID: 496722
URI: http://eprints.soton.ac.uk/id/eprint/496722
PURE UUID: 8f66ec8e-6353-470d-91d4-92d485c298ab
ORCID for Long Wu: ORCID iD orcid.org/0009-0006-8578-7755
ORCID for Jae-Wook Kim: ORCID iD orcid.org/0000-0003-0476-2574

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Date deposited: 07 Jan 2025 22:08
Last modified: 10 Jan 2025 03:04

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Contributors

Author: Long Wu ORCID iD
Author: Jae-Wook Kim ORCID iD

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