Sound extrapolation methods for turbulent flows based on indirect acoustic variables

Siyang Zhong, Xin Zhang, Christopher L. Morfey, Richard Sandberg, Ryu Fattah

Research output: Chapter in book / Conference proceedingConference article published in proceeding or bookAcademic researchpeer-review

1 Citation (Scopus)

Abstract

In computing sound radiation from a turbulent flow, the far-field directivity solutions based on sound extrapolation methods can be contaminated if the expensive volume integrals are neglected while the non-acoustic fluctuations are collected on the integration surface. In earlier work by the first two authors, a sound extrapolation method was developed by filtering out the eddies before the far-field computation. A convection operator Dc was applied on the pressure fluctuation p′ under the assumption that the motion of the eddies is mainly convected by the mean flow, as indicated by Taylor's hypothesis. Good results were obtained when the method was applied to typical aeroacoustic problems. In this work, we develop two more formulations using alternative indirect acoustic variables. The first method is based on the convection operator Dc to the velocity fluctuation u′ that seems to be more relevant to Taylor's hypothesis. The second method uses u′ = ∇ ·u′ as the acoustic variable based on the fact that the sound waves are related to the compressive process of a fluid medium. The methods are studied using different benchmark problems and practical aeroacoustic applications. It is shown that all methods work well for the two-dimensional (2D) convecting vortex, an acoustic monopole in uniform flow and the at plate - gust interaction problem. However, when the three methods are applied to vortex- shedding noise and to co-owing jet noise, the original method based on Dcp′ shows least sensitivity to choice of integration surface, and results obtained using different integration surfaces with the variables v′ and Dcu′ are inconsistent. It is found that the reason for the poor performance is that non-acoustic components are also contained in the indirect variables v′ and Dcu′ on the integration surfaces.

Original languageEnglish
Title of host publication2018 AIAA/CEAS Aeroacoustics Conference
PublisherAmerican Institute of Aeronautics and Astronautics Inc. (AIAA)
ISBN (Print)9781624105609
DOIs
Publication statusPublished - 1 Jan 2018
Externally publishedYes
EventAIAA/CEAS Aeroacoustics Conference, 2018 - Atlanta, United States
Duration: 25 Jun 201829 Jun 2018

Publication series

Name2018 AIAA/CEAS Aeroacoustics Conference

Conference

ConferenceAIAA/CEAS Aeroacoustics Conference, 2018
Country/TerritoryUnited States
CityAtlanta
Period25/06/1829/06/18

ASJC Scopus subject areas

  • Electrical and Electronic Engineering
  • Aerospace Engineering

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