Noise transmission through aircraft panels
This paper describes analytical and experimental studies of noise transmission through aircraft panels. The theoretical solutions of the governing acoustic-structural equations are developed utilizing modal decomposition and a Galerkin-type procedure. Single, discretely stiffened, and double wall pa...
Gespeichert in:
Veröffentlicht in: | Journal of aircraft 1985-04, Vol.22 (4), p.303-310 |
---|---|
Hauptverfasser: | , , |
Format: | Artikel |
Sprache: | eng |
Schlagworte: | |
Online-Zugang: | Volltext |
Tags: |
Tag hinzufügen
Keine Tags, Fügen Sie den ersten Tag hinzu!
|
container_end_page | 310 |
---|---|
container_issue | 4 |
container_start_page | 303 |
container_title | Journal of aircraft |
container_volume | 22 |
creator | Vaicaitis, R Grosveld, F. W Mixson, J. S |
description | This paper describes analytical and experimental studies of noise transmission through aircraft panels. The theoretical solutions of the governing acoustic-structural equations are developed utilizing modal decomposition and a Galerkin-type procedure. Single, discretely stiffened, and double wall panels are considered. Theoretical predictions are compared with experimental measurements. |
doi_str_mv | 10.2514/3.45124 |
format | Article |
fullrecord | <record><control><sourceid>proquest_aiaa_</sourceid><recordid>TN_cdi_aiaa_journals_3_45124_pdf_fulltext</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>14116792</sourcerecordid><originalsourceid>FETCH-LOGICAL-a369t-31906c907af6b0a6e40310b9b98f30ef19b0bd67a17b9f281c4b03720ff933c03</originalsourceid><addsrcrecordid>eNqFkM1KxDAYRYMoOI7iC7joQhSFjt-XpPlZyuAfDLrRdUg7idOh045JCvr2VjtLwdVd3MPhcgk5RZjRAvkNm_ECKd8jEywYy5kSap9MACjmSgh9SI5iXAOAAikn5Pq5q6PLUrBt3NQx1l2bpVXo-vdVZutQBetTtrWta-IxOfC2ie5kl1Pydn_3On_MFy8PT_PbRW6Z0ClnqEFUGqT1ogQrHAeGUOpSK8_AedQllEshLcpSe6qw4iUwScF7zVgFbEouRu82dB-9i8kMwyrXNMOKro-GcqE4p_gviBxRSE0H8HIEq9DFGJw321BvbPgyCObnNMPM72kDeTaSrY3WtCkMFq0KAC4R5FCfj7WtrTXrrg_t8MQflqu_sF1ttktvfN80yX0m9g1F0X7f</addsrcrecordid><sourcetype>Aggregation Database</sourcetype><iscdi>true</iscdi><recordtype>article</recordtype><pqid>14116792</pqid></control><display><type>article</type><title>Noise transmission through aircraft panels</title><source>NASA Technical Reports Server</source><source>Alma/SFX Local Collection</source><creator>Vaicaitis, R ; Grosveld, F. W ; Mixson, J. S</creator><creatorcontrib>Vaicaitis, R ; Grosveld, F. W ; Mixson, J. S</creatorcontrib><description>This paper describes analytical and experimental studies of noise transmission through aircraft panels. The theoretical solutions of the governing acoustic-structural equations are developed utilizing modal decomposition and a Galerkin-type procedure. Single, discretely stiffened, and double wall panels are considered. Theoretical predictions are compared with experimental measurements.</description><identifier>ISSN: 0021-8669</identifier><identifier>EISSN: 1533-3868</identifier><identifier>DOI: 10.2514/3.45124</identifier><language>eng</language><publisher>Legacy CDMS</publisher><subject>acoustic measurements ; acoustic variables measurement ; Acoustics ; aircraft ; fluid mechanics ; noise ; noise levels ; panels ; structural parts</subject><ispartof>Journal of aircraft, 1985-04, Vol.22 (4), p.303-310</ispartof><lds50>peer_reviewed</lds50><woscitedreferencessubscribed>false</woscitedreferencessubscribed><citedby>FETCH-LOGICAL-a369t-31906c907af6b0a6e40310b9b98f30ef19b0bd67a17b9f281c4b03720ff933c03</citedby><cites>FETCH-LOGICAL-a369t-31906c907af6b0a6e40310b9b98f30ef19b0bd67a17b9f281c4b03720ff933c03</cites></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><link.rule.ids>314,776,780,27901,27902</link.rule.ids></links><search><creatorcontrib>Vaicaitis, R</creatorcontrib><creatorcontrib>Grosveld, F. W</creatorcontrib><creatorcontrib>Mixson, J. S</creatorcontrib><title>Noise transmission through aircraft panels</title><title>Journal of aircraft</title><description>This paper describes analytical and experimental studies of noise transmission through aircraft panels. The theoretical solutions of the governing acoustic-structural equations are developed utilizing modal decomposition and a Galerkin-type procedure. Single, discretely stiffened, and double wall panels are considered. Theoretical predictions are compared with experimental measurements.</description><subject>acoustic measurements</subject><subject>acoustic variables measurement</subject><subject>Acoustics</subject><subject>aircraft</subject><subject>fluid mechanics</subject><subject>noise</subject><subject>noise levels</subject><subject>panels</subject><subject>structural parts</subject><issn>0021-8669</issn><issn>1533-3868</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>1985</creationdate><recordtype>article</recordtype><sourceid>CYI</sourceid><recordid>eNqFkM1KxDAYRYMoOI7iC7joQhSFjt-XpPlZyuAfDLrRdUg7idOh045JCvr2VjtLwdVd3MPhcgk5RZjRAvkNm_ECKd8jEywYy5kSap9MACjmSgh9SI5iXAOAAikn5Pq5q6PLUrBt3NQx1l2bpVXo-vdVZutQBetTtrWta-IxOfC2ie5kl1Pydn_3On_MFy8PT_PbRW6Z0ClnqEFUGqT1ogQrHAeGUOpSK8_AedQllEshLcpSe6qw4iUwScF7zVgFbEouRu82dB-9i8kMwyrXNMOKro-GcqE4p_gviBxRSE0H8HIEq9DFGJw321BvbPgyCObnNMPM72kDeTaSrY3WtCkMFq0KAC4R5FCfj7WtrTXrrg_t8MQflqu_sF1ttktvfN80yX0m9g1F0X7f</recordid><startdate>19850401</startdate><enddate>19850401</enddate><creator>Vaicaitis, R</creator><creator>Grosveld, F. W</creator><creator>Mixson, J. S</creator><scope>CYE</scope><scope>CYI</scope><scope>AAYXX</scope><scope>CITATION</scope><scope>7T2</scope><scope>7TC</scope><scope>7U2</scope><scope>C1K</scope><scope>8FD</scope><scope>H8D</scope><scope>L7M</scope></search><sort><creationdate>19850401</creationdate><title>Noise transmission through aircraft panels</title><author>Vaicaitis, R ; Grosveld, F. W ; Mixson, J. S</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-a369t-31906c907af6b0a6e40310b9b98f30ef19b0bd67a17b9f281c4b03720ff933c03</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>1985</creationdate><topic>acoustic measurements</topic><topic>acoustic variables measurement</topic><topic>Acoustics</topic><topic>aircraft</topic><topic>fluid mechanics</topic><topic>noise</topic><topic>noise levels</topic><topic>panels</topic><topic>structural parts</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Vaicaitis, R</creatorcontrib><creatorcontrib>Grosveld, F. W</creatorcontrib><creatorcontrib>Mixson, J. S</creatorcontrib><collection>NASA Scientific and Technical Information</collection><collection>NASA Technical Reports Server</collection><collection>CrossRef</collection><collection>Health and Safety Science Abstracts (Full archive)</collection><collection>Mechanical Engineering Abstracts</collection><collection>Safety Science and Risk</collection><collection>Environmental Sciences and Pollution Management</collection><collection>Technology Research Database</collection><collection>Aerospace Database</collection><collection>Advanced Technologies Database with Aerospace</collection><jtitle>Journal of aircraft</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Vaicaitis, R</au><au>Grosveld, F. W</au><au>Mixson, J. S</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Noise transmission through aircraft panels</atitle><jtitle>Journal of aircraft</jtitle><date>1985-04-01</date><risdate>1985</risdate><volume>22</volume><issue>4</issue><spage>303</spage><epage>310</epage><pages>303-310</pages><issn>0021-8669</issn><eissn>1533-3868</eissn><abstract>This paper describes analytical and experimental studies of noise transmission through aircraft panels. The theoretical solutions of the governing acoustic-structural equations are developed utilizing modal decomposition and a Galerkin-type procedure. Single, discretely stiffened, and double wall panels are considered. Theoretical predictions are compared with experimental measurements.</abstract><cop>Legacy CDMS</cop><doi>10.2514/3.45124</doi><tpages>8</tpages></addata></record> |
fulltext | fulltext |
identifier | ISSN: 0021-8669 |
ispartof | Journal of aircraft, 1985-04, Vol.22 (4), p.303-310 |
issn | 0021-8669 1533-3868 |
language | eng |
recordid | cdi_aiaa_journals_3_45124_pdf_fulltext |
source | NASA Technical Reports Server; Alma/SFX Local Collection |
subjects | acoustic measurements acoustic variables measurement Acoustics aircraft fluid mechanics noise noise levels panels structural parts |
title | Noise transmission through aircraft panels |
url | https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-02-07T02%3A11%3A06IST&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=Noise%20transmission%20through%20aircraft%20panels&rft.jtitle=Journal%20of%20aircraft&rft.au=Vaicaitis,%20R&rft.date=1985-04-01&rft.volume=22&rft.issue=4&rft.spage=303&rft.epage=310&rft.pages=303-310&rft.issn=0021-8669&rft.eissn=1533-3868&rft_id=info:doi/10.2514/3.45124&rft_dat=%3Cproquest_aiaa_%3E14116792%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=14116792&rft_id=info:pmid/&rfr_iscdi=true |