Validation of an Improved Experimental Method for Use in Impedance Eduction
Results from impedance eduction methods developed by NASA Langley Research Center are used throughout the acoustic liner community. Occasional anomalies persist with these methods at frequencies where the liner produces minimal attenuation. An approach to educe impedance spectra with increased confi...
Gespeichert in:
Veröffentlicht in: | AIAA journal 2013-01, Vol.51 (1), p.186-199 |
---|---|
Hauptverfasser: | , |
Format: | Artikel |
Sprache: | eng |
Schlagworte: | |
Online-Zugang: | Volltext |
Tags: |
Tag hinzufügen
Keine Tags, Fügen Sie den ersten Tag hinzu!
|
container_end_page | 199 |
---|---|
container_issue | 1 |
container_start_page | 186 |
container_title | AIAA journal |
container_volume | 51 |
creator | Jones, M. G Watson, W. R |
description | Results from impedance eduction methods developed by NASA Langley Research Center are used throughout the acoustic liner community. Occasional anomalies persist with these methods at frequencies where the liner produces minimal attenuation. An approach to educe impedance spectra with increased confidence is demonstrated, by combining results from successive tests with different cavity depths. First, a raylometer is used to measure the DC flow resistance of three wire-mesh facesheets. These facesheets are then mounted onto frames and a normal incidence tube is used to determine their respective acoustic impedance spectra. Next, each facesheet is successively mounted onto three frames with different cavity depths, and a grazing flow impedance tube is used to educe their respective acoustic impedance spectra with and without mean flow. Since the resonance frequency varies with cavity depth, each sample provides robust results over a different frequency range. Hence, a combination of results can be used to determine the facesheet acoustic resistance. When combined with the acoustic reactance (weakly dependent on the source sound pressure level and grazing flow Mach number), the acoustic impedance can be educed with increased confidence. Representative test results are discussed, and the complete database is available in electronic format upon request. |
doi_str_mv | 10.2514/1.J051705 |
format | Article |
fullrecord | <record><control><sourceid>proquest_aiaa_</sourceid><recordid>TN_cdi_proquest_miscellaneous_1349465478</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>1349465478</sourcerecordid><originalsourceid>FETCH-LOGICAL-a351t-8ecbeeddddbf110feb54e6f5edf6edf371911bd080aad8d19333f575cca8ff483</originalsourceid><addsrcrecordid>eNplkFFLw0AMxw9RcE4f_AYHouhD56XX67WPMqZOJ7448a2kvRx2dO3staLf3psbIhoIIfDLP8mfsWMQo1BBdAmjO6FAC7XDBqCkDGSiXnbZQAgBAUQq3GcHzi18F-oEBuz-GavSYFc2NW8sx5pPl6u2eSfDJx8rassl1R1W_IG618Zw27R87oiX3xwZrAviE9MXa4FDtmexcnS0rUM2v548jW-D2ePNdHw1C1Aq6IKEipzI-MgtgLCUq4hiq8jY2KfUkALkRiQC0SQGUimlVVoVBSbWRokcsvONrj_0rSfXZcvSFVRVWFPTuwxklEaxivQaPfmDLpq-rf11GYRxClorLTx1saGKtnGuJZut_OPYfmYgsrWtGWRbWz17ulVEV2BlW29B6X4GQi3DSEnw3NmGwxLx19Z_gl_bWoJo</addsrcrecordid><sourcetype>Aggregation Database</sourcetype><iscdi>true</iscdi><recordtype>article</recordtype><pqid>1269177570</pqid></control><display><type>article</type><title>Validation of an Improved Experimental Method for Use in Impedance Eduction</title><source>Alma/SFX Local Collection</source><creator>Jones, M. G ; Watson, W. R</creator><creatorcontrib>Jones, M. G ; Watson, W. R</creatorcontrib><description>Results from impedance eduction methods developed by NASA Langley Research Center are used throughout the acoustic liner community. Occasional anomalies persist with these methods at frequencies where the liner produces minimal attenuation. An approach to educe impedance spectra with increased confidence is demonstrated, by combining results from successive tests with different cavity depths. First, a raylometer is used to measure the DC flow resistance of three wire-mesh facesheets. These facesheets are then mounted onto frames and a normal incidence tube is used to determine their respective acoustic impedance spectra. Next, each facesheet is successively mounted onto three frames with different cavity depths, and a grazing flow impedance tube is used to educe their respective acoustic impedance spectra with and without mean flow. Since the resonance frequency varies with cavity depth, each sample provides robust results over a different frequency range. Hence, a combination of results can be used to determine the facesheet acoustic resistance. When combined with the acoustic reactance (weakly dependent on the source sound pressure level and grazing flow Mach number), the acoustic impedance can be educed with increased confidence. Representative test results are discussed, and the complete database is available in electronic format upon request.</description><identifier>ISSN: 0001-1452</identifier><identifier>EISSN: 1533-385X</identifier><identifier>DOI: 10.2514/1.J051705</identifier><identifier>CODEN: AIAJAH</identifier><language>eng</language><publisher>Reston, VA: American Institute of Aeronautics and Astronautics</publisher><subject>Acoustic impedance ; Acoustical measurements and instrumentation ; Acoustics ; Aerodynamics ; Confidence ; Exact sciences and technology ; Frequencies ; Fundamental areas of phenomenology (including applications) ; Grazing flow ; Holes ; Impedance ; Noise: its effects and control ; Physics ; Pressure ; Spectra ; Tubes</subject><ispartof>AIAA journal, 2013-01, Vol.51 (1), p.186-199</ispartof><rights>This material is declared a work of the U.S. Government and is not subject to copyright protection in the United States. Copies of this paper may be made for personal or internal use, on condition that the copier pay the $10.00 per-copy fee to the Copyright Clearance Center, Inc., 222 Rosewood Drive, Danvers, MA 01923; include the code and $10.00 in correspondence with the CCC.</rights><rights>2014 INIST-CNRS</rights><rights>Copyright American Institute of Aeronautics and Astronautics Jan 2013</rights><lds50>peer_reviewed</lds50><woscitedreferencessubscribed>false</woscitedreferencessubscribed><citedby>FETCH-LOGICAL-a351t-8ecbeeddddbf110feb54e6f5edf6edf371911bd080aad8d19333f575cca8ff483</citedby><cites>FETCH-LOGICAL-a351t-8ecbeeddddbf110feb54e6f5edf6edf371911bd080aad8d19333f575cca8ff483</cites></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><link.rule.ids>315,781,785,4025,27928,27929,27930</link.rule.ids><backlink>$$Uhttp://pascal-francis.inist.fr/vibad/index.php?action=getRecordDetail&idt=27324531$$DView record in Pascal Francis$$Hfree_for_read</backlink></links><search><creatorcontrib>Jones, M. G</creatorcontrib><creatorcontrib>Watson, W. R</creatorcontrib><title>Validation of an Improved Experimental Method for Use in Impedance Eduction</title><title>AIAA journal</title><description>Results from impedance eduction methods developed by NASA Langley Research Center are used throughout the acoustic liner community. Occasional anomalies persist with these methods at frequencies where the liner produces minimal attenuation. An approach to educe impedance spectra with increased confidence is demonstrated, by combining results from successive tests with different cavity depths. First, a raylometer is used to measure the DC flow resistance of three wire-mesh facesheets. These facesheets are then mounted onto frames and a normal incidence tube is used to determine their respective acoustic impedance spectra. Next, each facesheet is successively mounted onto three frames with different cavity depths, and a grazing flow impedance tube is used to educe their respective acoustic impedance spectra with and without mean flow. Since the resonance frequency varies with cavity depth, each sample provides robust results over a different frequency range. Hence, a combination of results can be used to determine the facesheet acoustic resistance. When combined with the acoustic reactance (weakly dependent on the source sound pressure level and grazing flow Mach number), the acoustic impedance can be educed with increased confidence. Representative test results are discussed, and the complete database is available in electronic format upon request.</description><subject>Acoustic impedance</subject><subject>Acoustical measurements and instrumentation</subject><subject>Acoustics</subject><subject>Aerodynamics</subject><subject>Confidence</subject><subject>Exact sciences and technology</subject><subject>Frequencies</subject><subject>Fundamental areas of phenomenology (including applications)</subject><subject>Grazing flow</subject><subject>Holes</subject><subject>Impedance</subject><subject>Noise: its effects and control</subject><subject>Physics</subject><subject>Pressure</subject><subject>Spectra</subject><subject>Tubes</subject><issn>0001-1452</issn><issn>1533-385X</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2013</creationdate><recordtype>article</recordtype><recordid>eNplkFFLw0AMxw9RcE4f_AYHouhD56XX67WPMqZOJ7448a2kvRx2dO3staLf3psbIhoIIfDLP8mfsWMQo1BBdAmjO6FAC7XDBqCkDGSiXnbZQAgBAUQq3GcHzi18F-oEBuz-GavSYFc2NW8sx5pPl6u2eSfDJx8rassl1R1W_IG618Zw27R87oiX3xwZrAviE9MXa4FDtmexcnS0rUM2v548jW-D2ePNdHw1C1Aq6IKEipzI-MgtgLCUq4hiq8jY2KfUkALkRiQC0SQGUimlVVoVBSbWRokcsvONrj_0rSfXZcvSFVRVWFPTuwxklEaxivQaPfmDLpq-rf11GYRxClorLTx1saGKtnGuJZut_OPYfmYgsrWtGWRbWz17ulVEV2BlW29B6X4GQi3DSEnw3NmGwxLx19Z_gl_bWoJo</recordid><startdate>201301</startdate><enddate>201301</enddate><creator>Jones, M. G</creator><creator>Watson, W. R</creator><general>American Institute of Aeronautics and Astronautics</general><scope>IQODW</scope><scope>AAYXX</scope><scope>CITATION</scope><scope>7TB</scope><scope>8FD</scope><scope>FR3</scope><scope>H8D</scope><scope>L7M</scope></search><sort><creationdate>201301</creationdate><title>Validation of an Improved Experimental Method for Use in Impedance Eduction</title><author>Jones, M. G ; Watson, W. R</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-a351t-8ecbeeddddbf110feb54e6f5edf6edf371911bd080aad8d19333f575cca8ff483</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2013</creationdate><topic>Acoustic impedance</topic><topic>Acoustical measurements and instrumentation</topic><topic>Acoustics</topic><topic>Aerodynamics</topic><topic>Confidence</topic><topic>Exact sciences and technology</topic><topic>Frequencies</topic><topic>Fundamental areas of phenomenology (including applications)</topic><topic>Grazing flow</topic><topic>Holes</topic><topic>Impedance</topic><topic>Noise: its effects and control</topic><topic>Physics</topic><topic>Pressure</topic><topic>Spectra</topic><topic>Tubes</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Jones, M. G</creatorcontrib><creatorcontrib>Watson, W. R</creatorcontrib><collection>Pascal-Francis</collection><collection>CrossRef</collection><collection>Mechanical & Transportation Engineering Abstracts</collection><collection>Technology Research Database</collection><collection>Engineering Research Database</collection><collection>Aerospace Database</collection><collection>Advanced Technologies Database with Aerospace</collection><jtitle>AIAA journal</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Jones, M. G</au><au>Watson, W. R</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Validation of an Improved Experimental Method for Use in Impedance Eduction</atitle><jtitle>AIAA journal</jtitle><date>2013-01</date><risdate>2013</risdate><volume>51</volume><issue>1</issue><spage>186</spage><epage>199</epage><pages>186-199</pages><issn>0001-1452</issn><eissn>1533-385X</eissn><coden>AIAJAH</coden><abstract>Results from impedance eduction methods developed by NASA Langley Research Center are used throughout the acoustic liner community. Occasional anomalies persist with these methods at frequencies where the liner produces minimal attenuation. An approach to educe impedance spectra with increased confidence is demonstrated, by combining results from successive tests with different cavity depths. First, a raylometer is used to measure the DC flow resistance of three wire-mesh facesheets. These facesheets are then mounted onto frames and a normal incidence tube is used to determine their respective acoustic impedance spectra. Next, each facesheet is successively mounted onto three frames with different cavity depths, and a grazing flow impedance tube is used to educe their respective acoustic impedance spectra with and without mean flow. Since the resonance frequency varies with cavity depth, each sample provides robust results over a different frequency range. Hence, a combination of results can be used to determine the facesheet acoustic resistance. When combined with the acoustic reactance (weakly dependent on the source sound pressure level and grazing flow Mach number), the acoustic impedance can be educed with increased confidence. Representative test results are discussed, and the complete database is available in electronic format upon request.</abstract><cop>Reston, VA</cop><pub>American Institute of Aeronautics and Astronautics</pub><doi>10.2514/1.J051705</doi><tpages>14</tpages></addata></record> |
fulltext | fulltext |
identifier | ISSN: 0001-1452 |
ispartof | AIAA journal, 2013-01, Vol.51 (1), p.186-199 |
issn | 0001-1452 1533-385X |
language | eng |
recordid | cdi_proquest_miscellaneous_1349465478 |
source | Alma/SFX Local Collection |
subjects | Acoustic impedance Acoustical measurements and instrumentation Acoustics Aerodynamics Confidence Exact sciences and technology Frequencies Fundamental areas of phenomenology (including applications) Grazing flow Holes Impedance Noise: its effects and control Physics Pressure Spectra Tubes |
title | Validation of an Improved Experimental Method for Use in Impedance Eduction |
url | https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2024-12-13T09%3A34%3A13IST&url_ver=Z39.88-2004&url_ctx_fmt=infofi/fmt:kev:mtx:ctx&rfr_id=info:sid/primo.exlibrisgroup.com:primo3-Article-proquest_aiaa_&rft_val_fmt=info:ofi/fmt:kev:mtx:journal&rft.genre=article&rft.atitle=Validation%20of%20an%20Improved%20Experimental%20Method%20for%20Use%20in%20Impedance%20Eduction&rft.jtitle=AIAA%20journal&rft.au=Jones,%20M.%20G&rft.date=2013-01&rft.volume=51&rft.issue=1&rft.spage=186&rft.epage=199&rft.pages=186-199&rft.issn=0001-1452&rft.eissn=1533-385X&rft.coden=AIAJAH&rft_id=info:doi/10.2514/1.J051705&rft_dat=%3Cproquest_aiaa_%3E1349465478%3C/proquest_aiaa_%3E%3Curl%3E%3C/url%3E&disable_directlink=true&sfx.directlink=off&sfx.report_link=0&rft_id=info:oai/&rft_pqid=1269177570&rft_id=info:pmid/&rfr_iscdi=true |