Conservative interpolation of aeroacoustic sources in a hybrid workflow applied to fan
Stefan J. Schoder, Clemens Junger, Michael Weitz, Manfred Kaltenbacher

TL;DR
This paper evaluates a conservative mesh-to-mesh interpolation method for aeroacoustic source transfer in hybrid simulations, demonstrating its accuracy and robustness for rotating systems like fans, with results aligning well with experimental data.
Contribution
It introduces and assesses a conservative cut-volume cell interpolation scheme for hybrid aeroacoustic workflows, improving accuracy over traditional methods for rotating systems.
Findings
The cut-volume cell interpolation provides accurate source transfer in hybrid aeroacoustic simulations.
The method shows robustness across different mesh configurations.
Simulation results agree well with experimental measurements.
Abstract
In low Mach number aeroacoustics, the well known disparity of scales makes it possible to apply efficient hybrid simulation models using different meshes for flow and acoustics, which leads to a powerful computational procedure. Our study applies the hybrid workflow to the computationally efficient perturbed convective wave equation with only one scalar unknown, the acoustic velocity potential. The workflow of this aeroacoustic approach is based on three steps: 1. perform unsteady incompressible flow computations on a sub-domain; 2. compute the acoustic sources; 3. simulate the acoustic field using a mesh specifically suited for computational aeroacoustics. In general, hybrid aeroacoustic methods seek for robust and conservative mesh-to-mesh transformation of the aeroacoustic sources while high computational efficiency is ensured. In this paper, we investigate the accuracy of a…
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Taxonomy
TopicsAerodynamics and Acoustics in Jet Flows · Fluid Dynamics and Turbulent Flows · Computational Fluid Dynamics and Aerodynamics
