2017
DOI: 10.1121/1.5006900
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Hermite regularization of the lattice Boltzmann method for open source computational aeroacoustics

Abstract: The lattice Boltzmann method (LBM) is emerging as a powerful engineering tool for aeroacoustic computations. However, the LBM has been shown to present accuracy and stability issues in the medium-low Mach number range, which is of interest for aeroacoustic applications. Several solutions have been proposed but are often too computationally expensive, do not retain the simplicity and the advantages typical of the LBM, or are not described well enough to be usable by the community due to proprietary software pol… Show more

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Cited by 30 publications
(29 citation statements)
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“…isothermal NS, thermal NS or even beyond NS 32 ). In this study, we use an optimized version of the standard LBM for aeroacoustic computations which is valid for isothermal fluid flow in the weakly compressible regimes ( ) 33 . In the case that pressure fluctuations are causing a significant temperature change, and hence affecting the sound speed, the model is expected to generate instabilities inducing divergence in the computational procedure.…”
Section: Methodsmentioning
confidence: 99%
“…isothermal NS, thermal NS or even beyond NS 32 ). In this study, we use an optimized version of the standard LBM for aeroacoustic computations which is valid for isothermal fluid flow in the weakly compressible regimes ( ) 33 . In the case that pressure fluctuations are causing a significant temperature change, and hence affecting the sound speed, the model is expected to generate instabilities inducing divergence in the computational procedure.…”
Section: Methodsmentioning
confidence: 99%
“…These methods achieve second-order spatial accuracy, yet resulting in a small numerical dissipation similar to a 6 â„Ž order optimized Navier-Stokes schemes [29], making LBM highly suitable for aeroacoustic predictions [30]. However classical BGK-LBM collision models can produce high frequency instabilities [31] when viscosity is low. As a consequence, a recursive and regularized BGK model (rrBGK-LBM) [32] is applied to maintain code stability with low numerical dissipation.…”
Section: Dataset Generationmentioning
confidence: 99%
“…This recursive approach was proven to increase the numerical stability of LBMs as compared to the original regularized collision model [69]. It was further shown to be competitive against state of the art Navier-Stokes and LBM solvers for the simulation of jet noise [70]. This confirmed its capability for high fidelity simulations, including computational aeroacoustics of moderate to high Reynods number flows.…”
Section: Introductionmentioning
confidence: 96%