Application Limits of Conservative Source Interpolation Methods Using a Low Mach Number Hybrid Aeroacoustic Workflow

DOI10.1142/s2591728520500322OpenAlexW3118222269MaRDI QIDQ6201461

Unnamed Author, Unnamed Author, S. Schoder, Unnamed Author, Klaus Roppert, Manfred Kaltenbacher, Unnamed Author

Publication date: 25 March 2024

Published in: Journal of Theoretical and Computational Acoustics (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1142/s2591728520500322

zbMATH Keywords

aeroacousticsacoustic analogyfan noisehybrid CAAbattery cooling fan

Mathematics Subject Classification ID

Hydro- and aero-acoustics (76Q05) Finite element, Rayleigh-Ritz and Galerkin methods for initial value and initial-boundary value problems involving PDEs (65M60)

Cites Work

• Unnamed Item
• Theory and applications of the multiquadric-biharmonic method. 20 years of discovery 1968-1988
• Conservative interpolation between volume meshes by local Galerkin projection
• Linearized acoustic perturbation equations for low Mach number flow with variable density and temperature
• An acoustic/viscous splitting technique for computational aeroacoustics
• Acoustic perturbation equations based on flow decomposition via source filtering
• Aeroacoustic modelling of low-speed flows
• A mortar-type finite element approach for embedding 1D beams into 3D solid volumes
• A radial basis function algorithm for simplified fluid-structure data transfer
• SPECTRAL FINITE ELEMENTS FOR COMPUTATIONAL AEROACOUSTICS USING ACOUSTIC PERTURBATION EQUATIONS
• Numerical simulation of flow-induced noise using LES/SAS and Lighthill's acoustic analogy
• Unified fluid–structure interpolation and mesh motion using radial basis functions

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