Prediction of low mach number turbulent flow noise using the splitting method

J. H. Seo, Young J. Moon

Research output: Chapter in Book/Report/Conference proceedingConference contribution

6 Citations (Scopus)

Abstract

A new methodology is proposed for the low Mach number turbulent flow noise prediction. Based on the hydrodynamic/acoustic splitting method, turbulent flow field is computed by an incompressible large eddy simulation(LES), while its acoustic field is predicted by the filtered perturbed-compressible- equations(FPCE). The FPCE which is derived from the incompressible and compressible LES equations does not require any particular modeling of the source term for turbulence. The present method is applied to turbulent noise prediction of flow past a circular cylinder at ReD=46000 and M=0.21. The predicted sound pressure level spectrum agrees fairly well with the experimental data of Boudet et al(AIAA Paper 2003-3217).

Original languageEnglish
Title of host publicationCollection of Technical Papers - 10th AIAA/CEAS Aeroacoustics Conference
PublisherAmerican Institute of Aeronautics and Astronautics Inc.
Pages699-709
Number of pages11
ISBN (Print)1563477130, 9781563477133
DOIs
Publication statusPublished - 2004
EventCollection of Technical Papers - 10th AIAA/CEAS Aeroacoustics Conference - Manchester, United Kingdom
Duration: 2004 May 102004 May 12

Publication series

NameCollection of Technical Papers - 10th AIAA/CEAS Aeroacoustics Conference
Volume1

Other

OtherCollection of Technical Papers - 10th AIAA/CEAS Aeroacoustics Conference
Country/TerritoryUnited Kingdom
CityManchester
Period04/5/1004/5/12

ASJC Scopus subject areas

  • Engineering(all)

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