20th AIAA/CEAS Aeroacoustics Conference 2014
DOI: 10.2514/6.2014-3101
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Towards Lattice-Boltzmann Prediction of Turbofan Engine Noise

Abstract: The goal of the present paper is to report verification and validation studies carried out by Exa Corporation in the framework of turbofan engine noise prediction through the hybrid Lattice-Boltzmann/Ffowcs-Williams & Hawkings approach (LB)-(FW-H). The underlying noise generation and propagation mechanisms related to the jet flow field and the fan are addressed separately by considering a series of elementary numerical experiments. As far as fan and jet noise generation is concerned, validation studies are per… Show more

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Cited by 27 publications
(24 citation statements)
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References 62 publications
(43 reference statements)
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“…LBM is a CFD technology developed over the last 30 years 13,14,15,16 and has been extensively validated for a wide variety of applications ranging from academic direct numerical simulation (DNS) cases to industrial flow problems in the fields of aerodynamics 17 and aeroacoustics. 8,18,19 In contrast to methods based on the Navier-Stokes (N-S) equations, LBM is based on a simpler and more general physics formulation. 13 The motivation behind the approach is to simulate a fluid at a microscopic level where the physics are simpler and more general than the macroscopic continuum approach taken by the N-S equations.…”
Section: Computational Approachmentioning
confidence: 99%
“…LBM is a CFD technology developed over the last 30 years 13,14,15,16 and has been extensively validated for a wide variety of applications ranging from academic direct numerical simulation (DNS) cases to industrial flow problems in the fields of aerodynamics 17 and aeroacoustics. 8,18,19 In contrast to methods based on the Navier-Stokes (N-S) equations, LBM is based on a simpler and more general physics formulation. 13 The motivation behind the approach is to simulate a fluid at a microscopic level where the physics are simpler and more general than the macroscopic continuum approach taken by the N-S equations.…”
Section: Computational Approachmentioning
confidence: 99%
“…where the colon symbol ':' stands for the full index contraction, H n for the Hermite polynomials of order n and ω = exp(−ξ 2 /2) for the associated Gaussian weight. For a complete review on the Hermite polynomials the interested reader is referred to Shan et al 49 The expansion coefficients a n are defined by a n (x, t) = f (x, ξ, t)H n (ξ)dξ (6) and correspond exactly to the velocity moments of the degree n. As a result, the observable macroscopic variables are directly obtained by the first three coefficients (four considering thermal fluids):…”
Section: A Standard and Optimized Lattice Boltzmann Dynamicsmentioning
confidence: 99%
“…Thus, it has opened promising perspectives for realistic applications. 10,11 The aim of this paper is to go one step further than previous LBM computations 8,9 and focus on a sensitivity analysis regarding various numerical parameters such as the subgrid scale model or the wall law components. In this purpose the newly developed Lattice Boltzmann solver called "LaBS" 12 will be used, as it allows the access to the sources of physical models, and gathers all numerical ingredients required for aeroacoustics.…”
Section: Introductionmentioning
confidence: 99%