Broadband sound power determination in aeroengine duct with respect to modal decomposition

In this paper an experimental technique for the decomposition of broadband ducted sound fields into their mode constituents is applied to a real low speed fan test rig, which enables not only the calculation of in-duct transmitted sound power for dominant tones, but also broadband noise over a wide...

Ausführliche Beschreibung

Gespeichert in:
Bibliographische Detailangaben
Hauptverfasser: Xu, Kunbo, Qiao, Weiyang
Format: Tagungsbericht
Sprache:eng
Online-Zugang:Volltext
Tags: Tag hinzufügen
Keine Tags, Fügen Sie den ersten Tag hinzu!
container_end_page
container_issue 1
container_start_page
container_title
container_volume 21
creator Xu, Kunbo
Qiao, Weiyang
description In this paper an experimental technique for the decomposition of broadband ducted sound fields into their mode constituents is applied to a real low speed fan test rig, which enables not only the calculation of in-duct transmitted sound power for dominant tones, but also broadband noise over a wide frequency range. The broadband mode analysis technique is based on spectral coherences using wall-flush installed pressure sensors as well as radial sensor rakes in the flow. The broadband sound power determination method was experimentally verified in a low speed fan test rig in Northwestern Polytechnical University. The experimental setup consists of a single-stage compressor in a flow duct. For mode detection 16 microphones were installed in the duct, a microphone mounted near the rotor was used as a reference sensor. Experimental results are presented for four operating conditions.
doi_str_mv 10.1121/1.4885102
format Conference Proceeding
fullrecord <record><control><sourceid>scitation</sourceid><recordid>TN_cdi_scitation_primary_10_1121_1_4885102</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>poma</sourcerecordid><originalsourceid>FETCH-LOGICAL-s140t-b9d139f43a4550334772ed47f7da5f3f9b4ab0887f8565ab11ae0c1f165f46d43</originalsourceid><addsrcrecordid>eNp9UMFKxDAUDILgunrwD3IWuuY1SZsedVFXWPCiIF7Ca5NoZNuUJOvi39vVBW9eZhiYGYYh5ALYAqCEK1gIpSSw8ojMoOFNoRh7OSGnKX0wVkFZyRl5vYkBTYuDoSlsJxzDzkZqbLax9wNmHwbqB4o2Bju8-cFSs-0y3fn8TqNNo51EDrQPBjdTrAv9GJLfx87IscNNsucHnpPnu9un5apYP94_LK_XRQLBctE2BnjjBEchJeNc1HVpjahdbVA67ppWYMuUqp2SlcQWAC3rwEElnaiM4HNy-dubOp9_Busx-h7jlwam909o0Icn_jN_hvhn1KNx_BuHy2LJ</addsrcrecordid><sourcetype>Enrichment Source</sourcetype><iscdi>true</iscdi><recordtype>conference_proceeding</recordtype></control><display><type>conference_proceeding</type><title>Broadband sound power determination in aeroengine duct with respect to modal decomposition</title><source>AIP Journals Complete</source><source>EZB-FREE-00999 freely available EZB journals</source><creator>Xu, Kunbo ; Qiao, Weiyang</creator><creatorcontrib>Xu, Kunbo ; Qiao, Weiyang</creatorcontrib><description>In this paper an experimental technique for the decomposition of broadband ducted sound fields into their mode constituents is applied to a real low speed fan test rig, which enables not only the calculation of in-duct transmitted sound power for dominant tones, but also broadband noise over a wide frequency range. The broadband mode analysis technique is based on spectral coherences using wall-flush installed pressure sensors as well as radial sensor rakes in the flow. The broadband sound power determination method was experimentally verified in a low speed fan test rig in Northwestern Polytechnical University. The experimental setup consists of a single-stage compressor in a flow duct. For mode detection 16 microphones were installed in the duct, a microphone mounted near the rotor was used as a reference sensor. Experimental results are presented for four operating conditions.</description><identifier>EISSN: 1939-800X</identifier><identifier>DOI: 10.1121/1.4885102</identifier><identifier>CODEN: PMARCW</identifier><language>eng</language><ispartof>Proceedings of Meetings on Acoustics, 2014, Vol.21 (1)</ispartof><rights>Acoustical Society of America</rights><lds50>peer_reviewed</lds50><woscitedreferencessubscribed>false</woscitedreferencessubscribed></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><linktohtml>$$Uhttps://pubs.aip.org/poma/article-lookup/doi/10.1121/1.4885102$$EHTML$$P50$$Gscitation$$H</linktohtml><link.rule.ids>208,309,310,780,784,789,790,794,4512,23930,23931,25140,27925,76384</link.rule.ids></links><search><creatorcontrib>Xu, Kunbo</creatorcontrib><creatorcontrib>Qiao, Weiyang</creatorcontrib><title>Broadband sound power determination in aeroengine duct with respect to modal decomposition</title><title>Proceedings of Meetings on Acoustics</title><description>In this paper an experimental technique for the decomposition of broadband ducted sound fields into their mode constituents is applied to a real low speed fan test rig, which enables not only the calculation of in-duct transmitted sound power for dominant tones, but also broadband noise over a wide frequency range. The broadband mode analysis technique is based on spectral coherences using wall-flush installed pressure sensors as well as radial sensor rakes in the flow. The broadband sound power determination method was experimentally verified in a low speed fan test rig in Northwestern Polytechnical University. The experimental setup consists of a single-stage compressor in a flow duct. For mode detection 16 microphones were installed in the duct, a microphone mounted near the rotor was used as a reference sensor. Experimental results are presented for four operating conditions.</description><issn>1939-800X</issn><fulltext>true</fulltext><rsrctype>conference_proceeding</rsrctype><creationdate>2014</creationdate><recordtype>conference_proceeding</recordtype><sourceid/><recordid>eNp9UMFKxDAUDILgunrwD3IWuuY1SZsedVFXWPCiIF7Ca5NoZNuUJOvi39vVBW9eZhiYGYYh5ALYAqCEK1gIpSSw8ojMoOFNoRh7OSGnKX0wVkFZyRl5vYkBTYuDoSlsJxzDzkZqbLax9wNmHwbqB4o2Bju8-cFSs-0y3fn8TqNNo51EDrQPBjdTrAv9GJLfx87IscNNsucHnpPnu9un5apYP94_LK_XRQLBctE2BnjjBEchJeNc1HVpjahdbVA67ppWYMuUqp2SlcQWAC3rwEElnaiM4HNy-dubOp9_Busx-h7jlwam909o0Icn_jN_hvhn1KNx_BuHy2LJ</recordid><startdate>20140613</startdate><enddate>20140613</enddate><creator>Xu, Kunbo</creator><creator>Qiao, Weiyang</creator><scope/></search><sort><creationdate>20140613</creationdate><title>Broadband sound power determination in aeroengine duct with respect to modal decomposition</title><author>Xu, Kunbo ; Qiao, Weiyang</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-s140t-b9d139f43a4550334772ed47f7da5f3f9b4ab0887f8565ab11ae0c1f165f46d43</frbrgroupid><rsrctype>conference_proceedings</rsrctype><prefilter>conference_proceedings</prefilter><language>eng</language><creationdate>2014</creationdate><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Xu, Kunbo</creatorcontrib><creatorcontrib>Qiao, Weiyang</creatorcontrib></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Xu, Kunbo</au><au>Qiao, Weiyang</au><format>book</format><genre>proceeding</genre><ristype>CONF</ristype><atitle>Broadband sound power determination in aeroengine duct with respect to modal decomposition</atitle><btitle>Proceedings of Meetings on Acoustics</btitle><date>2014-06-13</date><risdate>2014</risdate><volume>21</volume><issue>1</issue><eissn>1939-800X</eissn><coden>PMARCW</coden><abstract>In this paper an experimental technique for the decomposition of broadband ducted sound fields into their mode constituents is applied to a real low speed fan test rig, which enables not only the calculation of in-duct transmitted sound power for dominant tones, but also broadband noise over a wide frequency range. The broadband mode analysis technique is based on spectral coherences using wall-flush installed pressure sensors as well as radial sensor rakes in the flow. The broadband sound power determination method was experimentally verified in a low speed fan test rig in Northwestern Polytechnical University. The experimental setup consists of a single-stage compressor in a flow duct. For mode detection 16 microphones were installed in the duct, a microphone mounted near the rotor was used as a reference sensor. Experimental results are presented for four operating conditions.</abstract><doi>10.1121/1.4885102</doi><tpages>6</tpages></addata></record>
fulltext fulltext
identifier EISSN: 1939-800X
ispartof Proceedings of Meetings on Acoustics, 2014, Vol.21 (1)
issn 1939-800X
language eng
recordid cdi_scitation_primary_10_1121_1_4885102
source AIP Journals Complete; EZB-FREE-00999 freely available EZB journals
title Broadband sound power determination in aeroengine duct with respect to modal decomposition
url https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2024-12-23T14%3A14%3A40IST&url_ver=Z39.88-2004&url_ctx_fmt=infofi/fmt:kev:mtx:ctx&rfr_id=info:sid/primo.exlibrisgroup.com:primo3-Article-scitation&rft_val_fmt=info:ofi/fmt:kev:mtx:book&rft.genre=proceeding&rft.atitle=Broadband%20sound%20power%20determination%20in%20aeroengine%20duct%20with%20respect%20to%20modal%20decomposition&rft.btitle=Proceedings%20of%20Meetings%20on%20Acoustics&rft.au=Xu,%20Kunbo&rft.date=2014-06-13&rft.volume=21&rft.issue=1&rft.eissn=1939-800X&rft.coden=PMARCW&rft_id=info:doi/10.1121/1.4885102&rft_dat=%3Cscitation%3Epoma%3C/scitation%3E%3Curl%3E%3C/url%3E&disable_directlink=true&sfx.directlink=off&sfx.report_link=0&rft_id=info:oai/&rft_id=info:pmid/&rfr_iscdi=true