Por favor, use este identificador para citar o enlazar este ítem: http://repositorio.ufc.br/handle/riufc/62002
Tipo: Artigo de Periódico
Título : Two-point wavepacket modelling of jet noise
Autor : Maia, Igor Albuquerque
Jordan, Peter
Cavalieri, André Valdetaro Gomes
Jaunet, Vincent
Palabras clave : Fluid Mechanics;Jet noise;Wavepackets;Kinematic modelling
Fecha de publicación : 2019
Editorial : The Royal Society - https://royalsocietypublishing.org
Citación : 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.
Resumen en francés: 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)
Aparece en las colecciones: DEME - Artigos publicados em revista científica

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