Axisymmetric superdirectivity in subsonic jets
We present experimental results for the acoustic field of jets with Mach numbers between 0.35 and 0.6. An azimuthal ring array of six microphones, whose polar angle, $\theta $ , was progressively varied, allows the decomposition of the acoustic pressure into azimuthal Fourier modes. In agreement wi...
Gespeichert in:
Veröffentlicht in: | Journal of fluid mechanics 2012-08, Vol.704, p.388-420 |
---|---|
Hauptverfasser: | , , , |
Format: | Artikel |
Sprache: | eng |
Schlagworte: | |
Online-Zugang: | Volltext |
Tags: |
Tag hinzufügen
Keine Tags, Fügen Sie den ersten Tag hinzu!
|
container_end_page | 420 |
---|---|
container_issue | |
container_start_page | 388 |
container_title | Journal of fluid mechanics |
container_volume | 704 |
creator | Cavalieri, André V. G. Jordan, Peter Colonius, Tim Gervais, Yves |
description | We present experimental results for the acoustic field of jets with Mach numbers between 0.35 and 0.6. An azimuthal ring array of six microphones, whose polar angle,
$\theta $
, was progressively varied, allows the decomposition of the acoustic pressure into azimuthal Fourier modes. In agreement with past observations, the sound field for low polar angles (measured with respect to the jet axis) is found to be dominated by the axisymmetric mode, particularly at the peak Strouhal number. The axisymmetric mode of the acoustic field can be clearly associated with an axially non-compact source, in the form of a wavepacket: the sound pressure level for peak frequencies is found be superdirective for all Mach numbers considered, with exponential decay as a function of
$ \mathop{ (1\ensuremath{-} {M}_{c} \cos \theta )}\nolimits ^{2} $
, where
${M}_{c} $
is the Mach number based on the phase velocity
${U}_{c} $
of the convected wave. While the mode
$m= 1$
spectrum scales with Strouhal number, suggesting that its energy content is associated with turbulence scales, the axisymmetric mode scales with Helmholtz number – the ratio between source length scale and acoustic wavelength. The axisymmetric radiation has a stronger velocity dependence than the higher-order azimuthal modes, again in agreement with predictions of wavepacket models. We estimate the axial extent of the source of the axisymmetric component of the sound field to be of the order of six to eight jet diameters. This estimate is obtained in two different ways, using, respectively, the directivity shape and the velocity exponent of the sound radiation. The analysis furthermore shows that compressibility plays a significant role in the wavepacket dynamics, even at this low Mach number. Velocity fluctuations on the jet centreline are reduced as the Mach number is increased, an effect that must be accounted for in order to obtain a correct estimation of the velocity dependence of sound radiation. Finally, the higher-order azimuthal modes of the sound field are considered, and a model for the low-angle sound radiation by helical wavepackets is developed. The measured sound for azimuthal modes 1 and 2 at low Strouhal numbers is seen to correspond closely to the predicted directivity shapes. |
doi_str_mv | 10.1017/jfm.2012.247 |
format | Article |
fullrecord | <record><control><sourceid>proquest_cross</sourceid><recordid>TN_cdi_proquest_miscellaneous_1642269268</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><cupid>10_1017_jfm_2012_247</cupid><sourcerecordid>1642269268</sourcerecordid><originalsourceid>FETCH-LOGICAL-c403t-ad572b59b5d7d13ea2c4095790f174d0995936da7fe8f08b687ebf07269d10d13</originalsourceid><addsrcrecordid>eNptkEtLAzEUhYMoWKs7f0BBBBfOeJPJJJNlKb6g4EbXIZOHZJhHTWbE_ntTWkTE1YVzv3Pu5SB0iSHHgPld47qcACY5ofwIzTBlIuOMlsdoBkBIhjGBU3QWYwOACxB8hvLll4_brrNj8HoRp40NxgerR__px-3C90mr49CnZWPHeI5OnGqjvTjMOXp7uH9dPWXrl8fn1XKdaQrFmClTclKXoi4NN7iwiiRdlFyAw5waEKIUBTOKO1s5qGpWcVs74IQJgyE55uhmn7sJw8dk4yg7H7VtW9XbYYoSM0oSTFiV0Ks_aDNMoU_fSQyEccEI7KjbPaXDEGOwTm6C71TYJkjuypOpPLkrT6byEn59CFVRq9YF1WsffzyEYUEEpYnLD7Gqq4M37_b39X-CvwHponyX</addsrcrecordid><sourcetype>Aggregation Database</sourcetype><iscdi>true</iscdi><recordtype>article</recordtype><pqid>1026796208</pqid></control><display><type>article</type><title>Axisymmetric superdirectivity in subsonic jets</title><source>Cambridge University Press Journals Complete</source><creator>Cavalieri, André V. G. ; Jordan, Peter ; Colonius, Tim ; Gervais, Yves</creator><creatorcontrib>Cavalieri, André V. G. ; Jordan, Peter ; Colonius, Tim ; Gervais, Yves</creatorcontrib><description>We present experimental results for the acoustic field of jets with Mach numbers between 0.35 and 0.6. An azimuthal ring array of six microphones, whose polar angle,
$\theta $
, was progressively varied, allows the decomposition of the acoustic pressure into azimuthal Fourier modes. In agreement with past observations, the sound field for low polar angles (measured with respect to the jet axis) is found to be dominated by the axisymmetric mode, particularly at the peak Strouhal number. The axisymmetric mode of the acoustic field can be clearly associated with an axially non-compact source, in the form of a wavepacket: the sound pressure level for peak frequencies is found be superdirective for all Mach numbers considered, with exponential decay as a function of
$ \mathop{ (1\ensuremath{-} {M}_{c} \cos \theta )}\nolimits ^{2} $
, where
${M}_{c} $
is the Mach number based on the phase velocity
${U}_{c} $
of the convected wave. While the mode
$m= 1$
spectrum scales with Strouhal number, suggesting that its energy content is associated with turbulence scales, the axisymmetric mode scales with Helmholtz number – the ratio between source length scale and acoustic wavelength. The axisymmetric radiation has a stronger velocity dependence than the higher-order azimuthal modes, again in agreement with predictions of wavepacket models. We estimate the axial extent of the source of the axisymmetric component of the sound field to be of the order of six to eight jet diameters. This estimate is obtained in two different ways, using, respectively, the directivity shape and the velocity exponent of the sound radiation. The analysis furthermore shows that compressibility plays a significant role in the wavepacket dynamics, even at this low Mach number. Velocity fluctuations on the jet centreline are reduced as the Mach number is increased, an effect that must be accounted for in order to obtain a correct estimation of the velocity dependence of sound radiation. Finally, the higher-order azimuthal modes of the sound field are considered, and a model for the low-angle sound radiation by helical wavepackets is developed. The measured sound for azimuthal modes 1 and 2 at low Strouhal numbers is seen to correspond closely to the predicted directivity shapes.</description><identifier>ISSN: 0022-1120</identifier><identifier>EISSN: 1469-7645</identifier><identifier>DOI: 10.1017/jfm.2012.247</identifier><identifier>CODEN: JFLSA7</identifier><language>eng</language><publisher>Cambridge, UK: Cambridge University Press</publisher><subject>Acoustics ; Aeroacoustics, atmospheric sound ; Axisymmetric ; Estimates ; Exact sciences and technology ; Fluid dynamics ; Fluid mechanics ; Fundamental areas of phenomenology (including applications) ; Mach number ; Mathematical models ; Microphones ; Noise ; Noise (turbulence generated) ; Physics ; Sound fields ; Sound pressure ; Sound radiation ; Strouhal number ; Turbulent flows, convection, and heat transfer ; Velocity</subject><ispartof>Journal of fluid mechanics, 2012-08, Vol.704, p.388-420</ispartof><rights>Copyright © Cambridge University Press 2012</rights><rights>2015 INIST-CNRS</rights><rights>Copyright © Cambridge University Press 2012</rights><lds50>peer_reviewed</lds50><oa>free_for_read</oa><woscitedreferencessubscribed>false</woscitedreferencessubscribed><citedby>FETCH-LOGICAL-c403t-ad572b59b5d7d13ea2c4095790f174d0995936da7fe8f08b687ebf07269d10d13</citedby><cites>FETCH-LOGICAL-c403t-ad572b59b5d7d13ea2c4095790f174d0995936da7fe8f08b687ebf07269d10d13</cites></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><linktohtml>$$Uhttps://www.cambridge.org/core/product/identifier/S0022112012002479/type/journal_article$$EHTML$$P50$$Gcambridge$$H</linktohtml><link.rule.ids>164,314,780,784,27924,27925,55628</link.rule.ids><backlink>$$Uhttp://pascal-francis.inist.fr/vibad/index.php?action=getRecordDetail&idt=26192944$$DView record in Pascal Francis$$Hfree_for_read</backlink></links><search><creatorcontrib>Cavalieri, André V. G.</creatorcontrib><creatorcontrib>Jordan, Peter</creatorcontrib><creatorcontrib>Colonius, Tim</creatorcontrib><creatorcontrib>Gervais, Yves</creatorcontrib><title>Axisymmetric superdirectivity in subsonic jets</title><title>Journal of fluid mechanics</title><addtitle>J. Fluid Mech</addtitle><description>We present experimental results for the acoustic field of jets with Mach numbers between 0.35 and 0.6. An azimuthal ring array of six microphones, whose polar angle,
$\theta $
, was progressively varied, allows the decomposition of the acoustic pressure into azimuthal Fourier modes. In agreement with past observations, the sound field for low polar angles (measured with respect to the jet axis) is found to be dominated by the axisymmetric mode, particularly at the peak Strouhal number. The axisymmetric mode of the acoustic field can be clearly associated with an axially non-compact source, in the form of a wavepacket: the sound pressure level for peak frequencies is found be superdirective for all Mach numbers considered, with exponential decay as a function of
$ \mathop{ (1\ensuremath{-} {M}_{c} \cos \theta )}\nolimits ^{2} $
, where
${M}_{c} $
is the Mach number based on the phase velocity
${U}_{c} $
of the convected wave. While the mode
$m= 1$
spectrum scales with Strouhal number, suggesting that its energy content is associated with turbulence scales, the axisymmetric mode scales with Helmholtz number – the ratio between source length scale and acoustic wavelength. The axisymmetric radiation has a stronger velocity dependence than the higher-order azimuthal modes, again in agreement with predictions of wavepacket models. We estimate the axial extent of the source of the axisymmetric component of the sound field to be of the order of six to eight jet diameters. This estimate is obtained in two different ways, using, respectively, the directivity shape and the velocity exponent of the sound radiation. The analysis furthermore shows that compressibility plays a significant role in the wavepacket dynamics, even at this low Mach number. Velocity fluctuations on the jet centreline are reduced as the Mach number is increased, an effect that must be accounted for in order to obtain a correct estimation of the velocity dependence of sound radiation. Finally, the higher-order azimuthal modes of the sound field are considered, and a model for the low-angle sound radiation by helical wavepackets is developed. The measured sound for azimuthal modes 1 and 2 at low Strouhal numbers is seen to correspond closely to the predicted directivity shapes.</description><subject>Acoustics</subject><subject>Aeroacoustics, atmospheric sound</subject><subject>Axisymmetric</subject><subject>Estimates</subject><subject>Exact sciences and technology</subject><subject>Fluid dynamics</subject><subject>Fluid mechanics</subject><subject>Fundamental areas of phenomenology (including applications)</subject><subject>Mach number</subject><subject>Mathematical models</subject><subject>Microphones</subject><subject>Noise</subject><subject>Noise (turbulence generated)</subject><subject>Physics</subject><subject>Sound fields</subject><subject>Sound pressure</subject><subject>Sound radiation</subject><subject>Strouhal number</subject><subject>Turbulent flows, convection, and heat transfer</subject><subject>Velocity</subject><issn>0022-1120</issn><issn>1469-7645</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2012</creationdate><recordtype>article</recordtype><sourceid>8G5</sourceid><sourceid>ABUWG</sourceid><sourceid>AFKRA</sourceid><sourceid>AZQEC</sourceid><sourceid>BENPR</sourceid><sourceid>CCPQU</sourceid><sourceid>DWQXO</sourceid><sourceid>GNUQQ</sourceid><sourceid>GUQSH</sourceid><sourceid>M2O</sourceid><recordid>eNptkEtLAzEUhYMoWKs7f0BBBBfOeJPJJJNlKb6g4EbXIZOHZJhHTWbE_ntTWkTE1YVzv3Pu5SB0iSHHgPld47qcACY5ofwIzTBlIuOMlsdoBkBIhjGBU3QWYwOACxB8hvLll4_brrNj8HoRp40NxgerR__px-3C90mr49CnZWPHeI5OnGqjvTjMOXp7uH9dPWXrl8fn1XKdaQrFmClTclKXoi4NN7iwiiRdlFyAw5waEKIUBTOKO1s5qGpWcVs74IQJgyE55uhmn7sJw8dk4yg7H7VtW9XbYYoSM0oSTFiV0Ks_aDNMoU_fSQyEccEI7KjbPaXDEGOwTm6C71TYJkjuypOpPLkrT6byEn59CFVRq9YF1WsffzyEYUEEpYnLD7Gqq4M37_b39X-CvwHponyX</recordid><startdate>20120810</startdate><enddate>20120810</enddate><creator>Cavalieri, André V. G.</creator><creator>Jordan, Peter</creator><creator>Colonius, Tim</creator><creator>Gervais, Yves</creator><general>Cambridge University Press</general><scope>IQODW</scope><scope>AAYXX</scope><scope>CITATION</scope><scope>3V.</scope><scope>7TB</scope><scope>7U5</scope><scope>7UA</scope><scope>7XB</scope><scope>88I</scope><scope>8FD</scope><scope>8FE</scope><scope>8FG</scope><scope>8FK</scope><scope>8G5</scope><scope>ABJCF</scope><scope>ABUWG</scope><scope>AFKRA</scope><scope>ARAPS</scope><scope>AZQEC</scope><scope>BENPR</scope><scope>BGLVJ</scope><scope>BHPHI</scope><scope>BKSAR</scope><scope>C1K</scope><scope>CCPQU</scope><scope>DWQXO</scope><scope>F1W</scope><scope>FR3</scope><scope>GNUQQ</scope><scope>GUQSH</scope><scope>H8D</scope><scope>H96</scope><scope>HCIFZ</scope><scope>KR7</scope><scope>L.G</scope><scope>L6V</scope><scope>L7M</scope><scope>M2O</scope><scope>M2P</scope><scope>M7S</scope><scope>MBDVC</scope><scope>P5Z</scope><scope>P62</scope><scope>PCBAR</scope><scope>PQEST</scope><scope>PQQKQ</scope><scope>PQUKI</scope><scope>PTHSS</scope><scope>Q9U</scope><scope>S0W</scope></search><sort><creationdate>20120810</creationdate><title>Axisymmetric superdirectivity in subsonic jets</title><author>Cavalieri, André V. G. ; Jordan, Peter ; Colonius, Tim ; Gervais, Yves</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-c403t-ad572b59b5d7d13ea2c4095790f174d0995936da7fe8f08b687ebf07269d10d13</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2012</creationdate><topic>Acoustics</topic><topic>Aeroacoustics, atmospheric sound</topic><topic>Axisymmetric</topic><topic>Estimates</topic><topic>Exact sciences and technology</topic><topic>Fluid dynamics</topic><topic>Fluid mechanics</topic><topic>Fundamental areas of phenomenology (including applications)</topic><topic>Mach number</topic><topic>Mathematical models</topic><topic>Microphones</topic><topic>Noise</topic><topic>Noise (turbulence generated)</topic><topic>Physics</topic><topic>Sound fields</topic><topic>Sound pressure</topic><topic>Sound radiation</topic><topic>Strouhal number</topic><topic>Turbulent flows, convection, and heat transfer</topic><topic>Velocity</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Cavalieri, André V. G.</creatorcontrib><creatorcontrib>Jordan, Peter</creatorcontrib><creatorcontrib>Colonius, Tim</creatorcontrib><creatorcontrib>Gervais, Yves</creatorcontrib><collection>Pascal-Francis</collection><collection>CrossRef</collection><collection>ProQuest Central (Corporate)</collection><collection>Mechanical & Transportation Engineering Abstracts</collection><collection>Solid State and Superconductivity Abstracts</collection><collection>Water Resources Abstracts</collection><collection>ProQuest Central (purchase pre-March 2016)</collection><collection>Science Database (Alumni Edition)</collection><collection>Technology Research Database</collection><collection>ProQuest SciTech Collection</collection><collection>ProQuest Technology Collection</collection><collection>ProQuest Central (Alumni) (purchase pre-March 2016)</collection><collection>Research Library (Alumni Edition)</collection><collection>Materials Science & Engineering Collection</collection><collection>ProQuest Central (Alumni Edition)</collection><collection>ProQuest Central UK/Ireland</collection><collection>Advanced Technologies & Aerospace Collection</collection><collection>ProQuest Central Essentials</collection><collection>ProQuest Central</collection><collection>Technology Collection</collection><collection>Natural Science Collection</collection><collection>Earth, Atmospheric & Aquatic Science Collection</collection><collection>Environmental Sciences and Pollution Management</collection><collection>ProQuest One Community College</collection><collection>ProQuest Central Korea</collection><collection>ASFA: Aquatic Sciences and Fisheries Abstracts</collection><collection>Engineering Research Database</collection><collection>ProQuest Central Student</collection><collection>Research Library Prep</collection><collection>Aerospace Database</collection><collection>Aquatic Science & Fisheries Abstracts (ASFA) 2: Ocean Technology, Policy & Non-Living Resources</collection><collection>SciTech Premium Collection</collection><collection>Civil Engineering Abstracts</collection><collection>Aquatic Science & Fisheries Abstracts (ASFA) Professional</collection><collection>ProQuest Engineering Collection</collection><collection>Advanced Technologies Database with Aerospace</collection><collection>Research Library</collection><collection>Science Database</collection><collection>Engineering Database</collection><collection>Research Library (Corporate)</collection><collection>Advanced Technologies & Aerospace Database</collection><collection>ProQuest Advanced Technologies & Aerospace Collection</collection><collection>Earth, Atmospheric & Aquatic Science 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><collection>DELNET Engineering & Technology Collection</collection><jtitle>Journal of fluid mechanics</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Cavalieri, André V. G.</au><au>Jordan, Peter</au><au>Colonius, Tim</au><au>Gervais, Yves</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Axisymmetric superdirectivity in subsonic jets</atitle><jtitle>Journal of fluid mechanics</jtitle><addtitle>J. Fluid Mech</addtitle><date>2012-08-10</date><risdate>2012</risdate><volume>704</volume><spage>388</spage><epage>420</epage><pages>388-420</pages><issn>0022-1120</issn><eissn>1469-7645</eissn><coden>JFLSA7</coden><abstract>We present experimental results for the acoustic field of jets with Mach numbers between 0.35 and 0.6. An azimuthal ring array of six microphones, whose polar angle,
$\theta $
, was progressively varied, allows the decomposition of the acoustic pressure into azimuthal Fourier modes. In agreement with past observations, the sound field for low polar angles (measured with respect to the jet axis) is found to be dominated by the axisymmetric mode, particularly at the peak Strouhal number. The axisymmetric mode of the acoustic field can be clearly associated with an axially non-compact source, in the form of a wavepacket: the sound pressure level for peak frequencies is found be superdirective for all Mach numbers considered, with exponential decay as a function of
$ \mathop{ (1\ensuremath{-} {M}_{c} \cos \theta )}\nolimits ^{2} $
, where
${M}_{c} $
is the Mach number based on the phase velocity
${U}_{c} $
of the convected wave. While the mode
$m= 1$
spectrum scales with Strouhal number, suggesting that its energy content is associated with turbulence scales, the axisymmetric mode scales with Helmholtz number – the ratio between source length scale and acoustic wavelength. The axisymmetric radiation has a stronger velocity dependence than the higher-order azimuthal modes, again in agreement with predictions of wavepacket models. We estimate the axial extent of the source of the axisymmetric component of the sound field to be of the order of six to eight jet diameters. This estimate is obtained in two different ways, using, respectively, the directivity shape and the velocity exponent of the sound radiation. The analysis furthermore shows that compressibility plays a significant role in the wavepacket dynamics, even at this low Mach number. Velocity fluctuations on the jet centreline are reduced as the Mach number is increased, an effect that must be accounted for in order to obtain a correct estimation of the velocity dependence of sound radiation. Finally, the higher-order azimuthal modes of the sound field are considered, and a model for the low-angle sound radiation by helical wavepackets is developed. The measured sound for azimuthal modes 1 and 2 at low Strouhal numbers is seen to correspond closely to the predicted directivity shapes.</abstract><cop>Cambridge, UK</cop><pub>Cambridge University Press</pub><doi>10.1017/jfm.2012.247</doi><tpages>33</tpages><oa>free_for_read</oa></addata></record> |
fulltext | fulltext |
identifier | ISSN: 0022-1120 |
ispartof | Journal of fluid mechanics, 2012-08, Vol.704, p.388-420 |
issn | 0022-1120 1469-7645 |
language | eng |
recordid | cdi_proquest_miscellaneous_1642269268 |
source | Cambridge University Press Journals Complete |
subjects | Acoustics Aeroacoustics, atmospheric sound Axisymmetric Estimates Exact sciences and technology Fluid dynamics Fluid mechanics Fundamental areas of phenomenology (including applications) Mach number Mathematical models Microphones Noise Noise (turbulence generated) Physics Sound fields Sound pressure Sound radiation Strouhal number Turbulent flows, convection, and heat transfer Velocity |
title | Axisymmetric superdirectivity in subsonic jets |
url | https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-01-04T09%3A47%3A58IST&url_ver=Z39.88-2004&url_ctx_fmt=infofi/fmt:kev:mtx:ctx&rfr_id=info:sid/primo.exlibrisgroup.com:primo3-Article-proquest_cross&rft_val_fmt=info:ofi/fmt:kev:mtx:journal&rft.genre=article&rft.atitle=Axisymmetric%20superdirectivity%20in%20subsonic%20jets&rft.jtitle=Journal%20of%20fluid%20mechanics&rft.au=Cavalieri,%20Andr%C3%A9%20V.%20G.&rft.date=2012-08-10&rft.volume=704&rft.spage=388&rft.epage=420&rft.pages=388-420&rft.issn=0022-1120&rft.eissn=1469-7645&rft.coden=JFLSA7&rft_id=info:doi/10.1017/jfm.2012.247&rft_dat=%3Cproquest_cross%3E1642269268%3C/proquest_cross%3E%3Curl%3E%3C/url%3E&disable_directlink=true&sfx.directlink=off&sfx.report_link=0&rft_id=info:oai/&rft_pqid=1026796208&rft_id=info:pmid/&rft_cupid=10_1017_jfm_2012_247&rfr_iscdi=true |