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Numerical prediction of tonal noise generation in an inlet vaned low-speed axial fan using a hybrid aeroacoustic approach
Abstract This work presents a numerical prediction of the tonal noise generation in a single-stage, axial flow fan, using a hybrid approach that first calculates the noise sources (generation) using conventional computational fluid dynamics (CFD) techniques, and then estimates the noise level in the...
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Published in: | Proceedings of the Institution of Mechanical Engineers. Part C, Journal of mechanical engineering science Journal of mechanical engineering science, 2009-09, Vol.223 (9), p.2081-2098 |
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container_title | Proceedings of the Institution of Mechanical Engineers. Part C, Journal of mechanical engineering science |
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creator | Díaz, Argüelles K M Fernández, Oro J M Marigorta, E Blanco Morros, C Santolaria |
description | Abstract
This work presents a numerical prediction of the tonal noise generation in a single-stage, axial flow fan, using a hybrid approach that first calculates the noise sources (generation) using conventional computational fluid dynamics (CFD) techniques, and then estimates the noise level in the blower far-field region (propagation) by means of an aeroacoustic analogy. As a starting point, an unsteady three-dimensional full-annulus simulation of the internal flow is carried out, using a wall-modelled large eddy simulation (WMLES) scheme for the turbulence closure to identify the acoustic sources. A well-tested commercial CFD package, FLUENT, was employed for that purpose, so a complete set of unsteady forces exerted over the blades was calculated. Following, a generalization of Lighthill's aeroacoustic analogy, the so-called Ffowcs Williams and Hawkings (FFWH) aeroacoustic analogy, was numerically implemented using a C++algorithm to resolve an integral formulation of the free-field FFWH wave equation, where CFD data are included in the source terms. The major contribution was expected to be found in the estimation of the tonal noise levels, directly linked to the intensity of the stator—rotor interaction phenomena. Additionally, intensive experimental measurements in the noise propagation region of the fan were conducted, in order to validate the numerical study. A reasonable agreement was found in the tonal noise spectra, although important discrepancies appeared due to the attenuation produced by the fan casing, not considered in the numerical model. Although limitations in the current computational resources led to the use of a relatively coarse mesh in the CFD modelling, the numerical study provided valuable information about the particular influence of the tonal noise sources, estimating accordingly overall experimental trends, and showing the potentiality of numerical tools to deal with noise control for designers and researchers. |
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This work presents a numerical prediction of the tonal noise generation in a single-stage, axial flow fan, using a hybrid approach that first calculates the noise sources (generation) using conventional computational fluid dynamics (CFD) techniques, and then estimates the noise level in the blower far-field region (propagation) by means of an aeroacoustic analogy. As a starting point, an unsteady three-dimensional full-annulus simulation of the internal flow is carried out, using a wall-modelled large eddy simulation (WMLES) scheme for the turbulence closure to identify the acoustic sources. A well-tested commercial CFD package, FLUENT, was employed for that purpose, so a complete set of unsteady forces exerted over the blades was calculated. Following, a generalization of Lighthill's aeroacoustic analogy, the so-called Ffowcs Williams and Hawkings (FFWH) aeroacoustic analogy, was numerically implemented using a C++algorithm to resolve an integral formulation of the free-field FFWH wave equation, where CFD data are included in the source terms. The major contribution was expected to be found in the estimation of the tonal noise levels, directly linked to the intensity of the stator—rotor interaction phenomena. Additionally, intensive experimental measurements in the noise propagation region of the fan were conducted, in order to validate the numerical study. A reasonable agreement was found in the tonal noise spectra, although important discrepancies appeared due to the attenuation produced by the fan casing, not considered in the numerical model. Although limitations in the current computational resources led to the use of a relatively coarse mesh in the CFD modelling, the numerical study provided valuable information about the particular influence of the tonal noise sources, estimating accordingly overall experimental trends, and showing the potentiality of numerical tools to deal with noise control for designers and researchers.</description><identifier>ISSN: 0954-4062</identifier><identifier>EISSN: 2041-2983</identifier><identifier>DOI: 10.1243/09544062JMES1426</identifier><language>eng</language><publisher>London, England: SAGE Publications</publisher><subject>Acoustic measurement ; Acoustic noise ; Acoustics ; Aerodynamics ; Algorithms ; Attenuation ; Axial flow ; Blades ; Computational fluid dynamics ; Estimates ; Estimation ; Finite element method ; Fluid flow ; Hydraulic equipment ; Information dissemination ; Large eddy simulation ; Mathematical analysis ; Mathematical models ; Noise ; Noise control ; Noise prediction (aircraft) ; Noise propagation ; Noise spectra ; Simulation ; Sound sources ; Turbulence</subject><ispartof>Proceedings of the Institution of Mechanical Engineers. Part C, Journal of mechanical engineering science, 2009-09, Vol.223 (9), p.2081-2098</ispartof><rights>2009 Institution of Mechanical Engineers</rights><rights>Copyright Professional Engineering Publishing Ltd Sep 2009</rights><lds50>peer_reviewed</lds50><oa>free_for_read</oa><woscitedreferencessubscribed>false</woscitedreferencessubscribed><citedby>FETCH-LOGICAL-c450t-320ff7bb712ab578b40edfc328d7da051eec2ae193ba7bf404d8a8dace59e6a23</citedby><cites>FETCH-LOGICAL-c450t-320ff7bb712ab578b40edfc328d7da051eec2ae193ba7bf404d8a8dace59e6a23</cites></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><linktopdf>$$Uhttps://journals.sagepub.com/doi/pdf/10.1243/09544062JMES1426$$EPDF$$P50$$Gsage$$H</linktopdf><linktohtml>$$Uhttps://journals.sagepub.com/doi/10.1243/09544062JMES1426$$EHTML$$P50$$Gsage$$H</linktohtml><link.rule.ids>314,780,784,21912,27923,27924,45058,45446,79235</link.rule.ids></links><search><creatorcontrib>Díaz, Argüelles K M</creatorcontrib><creatorcontrib>Fernández, Oro J M</creatorcontrib><creatorcontrib>Marigorta, E Blanco</creatorcontrib><creatorcontrib>Morros, C Santolaria</creatorcontrib><title>Numerical prediction of tonal noise generation in an inlet vaned low-speed axial fan using a hybrid aeroacoustic approach</title><title>Proceedings of the Institution of Mechanical Engineers. Part C, Journal of mechanical engineering science</title><description>Abstract
This work presents a numerical prediction of the tonal noise generation in a single-stage, axial flow fan, using a hybrid approach that first calculates the noise sources (generation) using conventional computational fluid dynamics (CFD) techniques, and then estimates the noise level in the blower far-field region (propagation) by means of an aeroacoustic analogy. As a starting point, an unsteady three-dimensional full-annulus simulation of the internal flow is carried out, using a wall-modelled large eddy simulation (WMLES) scheme for the turbulence closure to identify the acoustic sources. A well-tested commercial CFD package, FLUENT, was employed for that purpose, so a complete set of unsteady forces exerted over the blades was calculated. Following, a generalization of Lighthill's aeroacoustic analogy, the so-called Ffowcs Williams and Hawkings (FFWH) aeroacoustic analogy, was numerically implemented using a C++algorithm to resolve an integral formulation of the free-field FFWH wave equation, where CFD data are included in the source terms. The major contribution was expected to be found in the estimation of the tonal noise levels, directly linked to the intensity of the stator—rotor interaction phenomena. Additionally, intensive experimental measurements in the noise propagation region of the fan were conducted, in order to validate the numerical study. A reasonable agreement was found in the tonal noise spectra, although important discrepancies appeared due to the attenuation produced by the fan casing, not considered in the numerical model. Although limitations in the current computational resources led to the use of a relatively coarse mesh in the CFD modelling, the numerical study provided valuable information about the particular influence of the tonal noise sources, estimating accordingly overall experimental trends, and showing the potentiality of numerical tools to deal with noise control for designers and researchers.</description><subject>Acoustic measurement</subject><subject>Acoustic noise</subject><subject>Acoustics</subject><subject>Aerodynamics</subject><subject>Algorithms</subject><subject>Attenuation</subject><subject>Axial flow</subject><subject>Blades</subject><subject>Computational fluid dynamics</subject><subject>Estimates</subject><subject>Estimation</subject><subject>Finite element method</subject><subject>Fluid flow</subject><subject>Hydraulic equipment</subject><subject>Information dissemination</subject><subject>Large eddy simulation</subject><subject>Mathematical analysis</subject><subject>Mathematical models</subject><subject>Noise</subject><subject>Noise control</subject><subject>Noise prediction (aircraft)</subject><subject>Noise propagation</subject><subject>Noise spectra</subject><subject>Simulation</subject><subject>Sound sources</subject><subject>Turbulence</subject><issn>0954-4062</issn><issn>2041-2983</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2009</creationdate><recordtype>article</recordtype><recordid>eNp1kUlPwzAQhS0EEqVw52iBxC3gLdsRVWUTywE4RxNn0rpK42AnQP89DuWAkJiDt_e98WiGkGPOzrlQ8oLlsVIsEXcP82euRLJDJoIpHok8k7tkMsrRqO-TA-9XLIRI4gnZPA5rdEZDQzuHldG9sS21Ne1tG95aazzSBbbo4FsxLYVxbbCn79BiRRv7EfkOwwk-TbDUQR-8aRcU6HJTOhMEdBa0HXxvNIWuG2_LQ7JXQ-Px6Gefkter-cvsJrp_ur6dXd5HWsWsj6RgdZ2WZcoFlHGalYphVWspsiqtgMUcUQtAnssS0rJWTFUZZBVojHNMQMgpOdvmDd--Dej7Ym28xqYJ1YeSCqnSLDQpCeDJH3BlBxe64AshVc6yjMkAnf4H8ZwzmYSIA8W2lHbWe4d10TmzBrcpOCvGcRV_xxUs0dbiYYG_kv7HfwHD_JbM</recordid><startdate>20090901</startdate><enddate>20090901</enddate><creator>Díaz, Argüelles K M</creator><creator>Fernández, Oro J M</creator><creator>Marigorta, E Blanco</creator><creator>Morros, C Santolaria</creator><general>SAGE Publications</general><general>SAGE PUBLICATIONS, INC</general><scope>AAYXX</scope><scope>CITATION</scope><scope>7TB</scope><scope>8FD</scope><scope>F28</scope><scope>FR3</scope><scope>3V.</scope><scope>7XB</scope><scope>88I</scope><scope>8AF</scope><scope>8AO</scope><scope>8FE</scope><scope>8FG</scope><scope>8FK</scope><scope>ABJCF</scope><scope>ABUWG</scope><scope>AFKRA</scope><scope>AZQEC</scope><scope>BENPR</scope><scope>BGLVJ</scope><scope>CCPQU</scope><scope>DWQXO</scope><scope>GNUQQ</scope><scope>HCIFZ</scope><scope>L6V</scope><scope>M2P</scope><scope>M7S</scope><scope>PQEST</scope><scope>PQQKQ</scope><scope>PQUKI</scope><scope>PTHSS</scope><scope>Q9U</scope></search><sort><creationdate>20090901</creationdate><title>Numerical prediction of tonal noise generation in an inlet vaned low-speed axial fan using a hybrid aeroacoustic approach</title><author>Díaz, Argüelles K M ; Fernández, Oro J M ; Marigorta, E Blanco ; Morros, C Santolaria</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-c450t-320ff7bb712ab578b40edfc328d7da051eec2ae193ba7bf404d8a8dace59e6a23</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2009</creationdate><topic>Acoustic measurement</topic><topic>Acoustic noise</topic><topic>Acoustics</topic><topic>Aerodynamics</topic><topic>Algorithms</topic><topic>Attenuation</topic><topic>Axial flow</topic><topic>Blades</topic><topic>Computational fluid dynamics</topic><topic>Estimates</topic><topic>Estimation</topic><topic>Finite element method</topic><topic>Fluid flow</topic><topic>Hydraulic equipment</topic><topic>Information dissemination</topic><topic>Large eddy simulation</topic><topic>Mathematical analysis</topic><topic>Mathematical models</topic><topic>Noise</topic><topic>Noise control</topic><topic>Noise prediction (aircraft)</topic><topic>Noise propagation</topic><topic>Noise spectra</topic><topic>Simulation</topic><topic>Sound sources</topic><topic>Turbulence</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Díaz, Argüelles K M</creatorcontrib><creatorcontrib>Fernández, Oro J M</creatorcontrib><creatorcontrib>Marigorta, E Blanco</creatorcontrib><creatorcontrib>Morros, C Santolaria</creatorcontrib><collection>CrossRef</collection><collection>Mechanical & Transportation Engineering Abstracts</collection><collection>Technology Research Database</collection><collection>ANTE: Abstracts in New Technology & Engineering</collection><collection>Engineering Research Database</collection><collection>ProQuest Central (Corporate)</collection><collection>ProQuest Central (purchase pre-March 2016)</collection><collection>Science Database (Alumni Edition)</collection><collection>STEM Database</collection><collection>ProQuest Pharma Collection</collection><collection>ProQuest SciTech Collection</collection><collection>ProQuest Technology Collection</collection><collection>ProQuest Central (Alumni) (purchase pre-March 2016)</collection><collection>Materials Science & Engineering Collection</collection><collection>ProQuest Central (Alumni)</collection><collection>ProQuest Central</collection><collection>ProQuest Central Essentials</collection><collection>AUTh Library subscriptions: ProQuest Central</collection><collection>Technology Collection</collection><collection>ProQuest One Community College</collection><collection>ProQuest Central</collection><collection>ProQuest Central Student</collection><collection>SciTech Premium Collection</collection><collection>ProQuest Engineering Collection</collection><collection>ProQuest Science Journals</collection><collection>Engineering Database</collection><collection>ProQuest One Academic Eastern Edition (DO NOT USE)</collection><collection>ProQuest One Academic</collection><collection>ProQuest One Academic UKI Edition</collection><collection>Engineering Collection</collection><collection>ProQuest Central Basic</collection><jtitle>Proceedings of the Institution of Mechanical Engineers. Part C, Journal of mechanical engineering science</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Díaz, Argüelles K M</au><au>Fernández, Oro J M</au><au>Marigorta, E Blanco</au><au>Morros, C Santolaria</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Numerical prediction of tonal noise generation in an inlet vaned low-speed axial fan using a hybrid aeroacoustic approach</atitle><jtitle>Proceedings of the Institution of Mechanical Engineers. Part C, Journal of mechanical engineering science</jtitle><date>2009-09-01</date><risdate>2009</risdate><volume>223</volume><issue>9</issue><spage>2081</spage><epage>2098</epage><pages>2081-2098</pages><issn>0954-4062</issn><eissn>2041-2983</eissn><abstract>Abstract
This work presents a numerical prediction of the tonal noise generation in a single-stage, axial flow fan, using a hybrid approach that first calculates the noise sources (generation) using conventional computational fluid dynamics (CFD) techniques, and then estimates the noise level in the blower far-field region (propagation) by means of an aeroacoustic analogy. As a starting point, an unsteady three-dimensional full-annulus simulation of the internal flow is carried out, using a wall-modelled large eddy simulation (WMLES) scheme for the turbulence closure to identify the acoustic sources. A well-tested commercial CFD package, FLUENT, was employed for that purpose, so a complete set of unsteady forces exerted over the blades was calculated. Following, a generalization of Lighthill's aeroacoustic analogy, the so-called Ffowcs Williams and Hawkings (FFWH) aeroacoustic analogy, was numerically implemented using a C++algorithm to resolve an integral formulation of the free-field FFWH wave equation, where CFD data are included in the source terms. The major contribution was expected to be found in the estimation of the tonal noise levels, directly linked to the intensity of the stator—rotor interaction phenomena. Additionally, intensive experimental measurements in the noise propagation region of the fan were conducted, in order to validate the numerical study. A reasonable agreement was found in the tonal noise spectra, although important discrepancies appeared due to the attenuation produced by the fan casing, not considered in the numerical model. Although limitations in the current computational resources led to the use of a relatively coarse mesh in the CFD modelling, the numerical study provided valuable information about the particular influence of the tonal noise sources, estimating accordingly overall experimental trends, and showing the potentiality of numerical tools to deal with noise control for designers and researchers.</abstract><cop>London, England</cop><pub>SAGE Publications</pub><doi>10.1243/09544062JMES1426</doi><tpages>18</tpages><oa>free_for_read</oa></addata></record> |
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subjects | Acoustic measurement Acoustic noise Acoustics Aerodynamics Algorithms Attenuation Axial flow Blades Computational fluid dynamics Estimates Estimation Finite element method Fluid flow Hydraulic equipment Information dissemination Large eddy simulation Mathematical analysis Mathematical models Noise Noise control Noise prediction (aircraft) Noise propagation Noise spectra Simulation Sound sources Turbulence |
title | Numerical prediction of tonal noise generation in an inlet vaned low-speed axial fan using a hybrid aeroacoustic approach |
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