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A low frequency model for the aeroacoustic scattering of cylindrical tube rows in cross-flow
Imperial Coll London, Dept Mech Engn, London SW72AZ, England.;Tech Univ Munich, Thermofluiddynam, 85747 Garching, Germany..
KTH, School of Engineering Sciences (SCI), Centres, Linné Flow Center, FLOW. KTH, School of Engineering Sciences (SCI), Engineering Mechanics, Fluid Mechanics and Engineering Acoustics. Marcus Wallenberg Lab Sound & Vibrat Res, Stockholm, Sweden..ORCID iD: 0000-0001-5757-3668
Imperial Coll London, Dept Mech Engn, London SW72AZ, England..
Imperial Coll London, Dept Mech Engn, London SW72AZ, England.;Southern Univ Sci & Technol, Dept Mech & Aerosp Engn, Shenzhen 518055, Peoples R China..
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2022 (English)In: Journal of Sound and Vibration, ISSN 0022-460X, E-ISSN 1095-8568, Vol. 527, p. 116806-, article id 116806Article in journal (Refereed) Published
Abstract [en]

Heat exchanger tube rows can influence the thermoacoustic instability behaviour of combustion systems since they act as both acoustic scatterers and unsteady heat sinks. Therefore, with careful tuning of their thermoacoustic properties, heat exchangers have the potential to act as passive control devices. In this work, we focus on (only) the acoustic scattering behaviour of heat exchanger tubes. We present a comparison of existing acoustic models for tube rows and slits, models for the latter having the advantage of incorporating frequency dependence. We then propose a new model that enables the adaptation of slit models for tube rows. This model is validated against experiments and Linearised Navier-Stokes Equations (LNSE) predictions for the transmission and reflection coefficients, including phase information. The model predictions show very good agreement with the experimental and numerical validations, especially for low frequencies (Strouhal number < 0.5, based on tube radius and excitation frequency), with mean differences less than 2% for the transmission coefficients (the reflection coefficient errors are somewhat larger since their magnitudes are very close to zero).

Place, publisher, year, edition, pages
ACADEMIC PRESS LTD- ELSEVIER SCIENCE LTD , 2022. Vol. 527, p. 116806-, article id 116806
Keywords [en]
Cummings-Fant equation, Acoustic scattering, Aeroacoustic models, Tube rows, Rectangular slits
National Category
Fluid Mechanics
Identifiers
URN: urn:nbn:se:kth:diva-313514DOI: 10.1016/j.jsv.2022.116806ISI: 000797026800005Scopus ID: 2-s2.0-85125255105OAI: oai:DiVA.org:kth-313514DiVA, id: diva2:1665276
Note

QC 20220607

Available from: 2022-06-07 Created: 2022-06-07 Last updated: 2025-02-09Bibliographically approved

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Na, WeiBoij, Susann

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Linné Flow Center, FLOWFluid Mechanics and Engineering Acoustics
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