Please use this identifier to cite or link to this item: http://repositorio.ufc.br/handle/riufc/62002
Type: Artigo de Periódico
Title: Two-point wavepacket modelling of jet noise
Authors: Maia, Igor Albuquerque
Jordan, Peter
Cavalieri, André Valdetaro Gomes
Jaunet, Vincent
Keywords: Fluid Mechanics;Jet noise;Wavepackets;Kinematic modelling
Issue Date: 2019
Publisher: The Royal Society - https://royalsocietypublishing.org
Citation: MAIA, Igor Albuquerque; JORDAN, Peter; CAVALIERI, André Valdetaro Gomes; JAUNET, Vincent. Two-point wavepacket modelling of jet noise. Proc. R. Soc., A 475, n. 2227, p. 01-27, 24 July 2019. DOI:https://doi.org/10.1098/rspa.2019.0199
Abstract: This paper is focused on the study of a kinematic wavepacket model for jet noise based on two-point statistics. The model contains physical parameters that define its structure in terms of wavenumber, envelope shape and coherence decay. These parameters, which are necessary to estimate the sound pressure levels radiated by the source, were educed from a large-eddy simulation database of a Mach 0.4, fully turbulent jet. The sound pressure levels predicted by the model were compared with acoustic data and the results show that when the parameters are carefully educed from the data, the sound pressure levels generated are in good agreement with experimentally measured values for low Strouhal numbers and polar angles. Furthermore, here we show that a correct representation of both coherence decay and wavepacket envelope shape are key aspects to an accurate sound prediction. A Spectral Proper Orthogonal Decomposition (SPOD) of the model source was also performed motivated by the search for a low-rank model capable of capturing the acoustic efficiency of the full source. It is shown that only a few SPOD modes are necessary to recover acoustically important wavepacket traits.
Abstract in French: Jet noise is a challenging and compelling problem in fluid mechanics, because of its environmental and societal relevance but also because of disagreements that exist in the aeroacoustics community regarding its theoretical basis. Despite nearly 70 years of research, there persists a lack of consensus regarding the flow structures responsible for sound generation. The first mathematical treatment for the jet noise problem was given by Lighthill [1] by means of his acoustic analogy. The main idea of the acoustic analogy is to rearrange the equations of motion as an inhomogeneous wave equation that separates the linear propagation of acoustic waves from a nonlinear inhomogeneous term composed of turbulent fluctuations that drive the sound field. In this framework, the turbulent field is replaced by an equivalent distribution of quadrupole sources whose statistical properties are related to those of the flow. Other acoustic analogies have since been proposed, for example, by Lilley [2] and Goldstein [3], that involve different source-propagator splits to deal with the effects of flow-acoustic interactions, but with the same central idea.[...]
URI: http://www.repositorio.ufc.br/handle/riufc/62002
ISSN: 1364-5021 (Print)
1471-2946 (Online)
Appears in Collections:DEME - Artigos publicados em revista científica

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