The Update of an Aerodynamic Wind-Tunnel for Aeroacoustics Testing

Detalhes bibliográficos
Autor(a) principal: Santana,Leandro Dantas
Data de Publicação: 2014
Outros Autores: Carmo,Micael, Catalano,Fernando Martini, Medeiros,Marcello A. F.
Tipo de documento: Artigo
Idioma: eng
Título da fonte: Journal of Aerospace Technology and Management (Online)
Texto Completo: http://old.scielo.br/scielo.php?script=sci_arttext&pid=S2175-91462014000200111
Resumo: ABSTRACT: This paper describes the update and characterization of a previously pure aerodynamics wind-tunnel into a facility able to simultaneously execute aerodynamics and aeroacoustics testing. It is demonstrated that the application of high-performance acoustic materials on strategic positions of the wind-tunnel circuit and punctual actions can substantially reduce the background-noise level. This paper shows efficient measures which resulted to broadband-noise reduction of up to 5 dB and practically complete removal of spectral tones. In addition, it is demonstrated that the applied acoustic treatment reduced the turbulence level, measured at the test-section at maximum operational velocity, from the previous 0.25% level to 0.21%. As a minor penalty, the acoustic treatment reduced the flow velocity in 2% for the same electric-power input. Finally, the work described in this paper resulted on a wind-tunnel with good flow quality and capacity for aeroacoustics testing.
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spelling The Update of an Aerodynamic Wind-Tunnel for Aeroacoustics TestingAeroacoustic testingWind-tunnel noiseWind-tunnel acoustic treatmentABSTRACT: This paper describes the update and characterization of a previously pure aerodynamics wind-tunnel into a facility able to simultaneously execute aerodynamics and aeroacoustics testing. It is demonstrated that the application of high-performance acoustic materials on strategic positions of the wind-tunnel circuit and punctual actions can substantially reduce the background-noise level. This paper shows efficient measures which resulted to broadband-noise reduction of up to 5 dB and practically complete removal of spectral tones. In addition, it is demonstrated that the applied acoustic treatment reduced the turbulence level, measured at the test-section at maximum operational velocity, from the previous 0.25% level to 0.21%. As a minor penalty, the acoustic treatment reduced the flow velocity in 2% for the same electric-power input. Finally, the work described in this paper resulted on a wind-tunnel with good flow quality and capacity for aeroacoustics testing.Departamento de Ciência e Tecnologia Aeroespacial2014-06-01info:eu-repo/semantics/articleinfo:eu-repo/semantics/publishedVersiontext/htmlhttp://old.scielo.br/scielo.php?script=sci_arttext&pid=S2175-91462014000200111Journal of Aerospace Technology and Management v.6 n.2 2014reponame:Journal of Aerospace Technology and Management (Online)instname:Departamento de Ciência e Tecnologia Aeroespacial (DCTA)instacron:DCTA10.5028/jatm.v6i2.308info:eu-repo/semantics/openAccessSantana,Leandro DantasCarmo,MicaelCatalano,Fernando MartiniMedeiros,Marcello A. F.eng2017-05-26T00:00:00Zoai:scielo:S2175-91462014000200111Revistahttp://www.jatm.com.br/ONGhttps://old.scielo.br/oai/scielo-oai.php||secretary@jatm.com.br2175-91461984-9648opendoar:2017-05-26T00:00Journal of Aerospace Technology and Management (Online) - Departamento de Ciência e Tecnologia Aeroespacial (DCTA)false
dc.title.none.fl_str_mv The Update of an Aerodynamic Wind-Tunnel for Aeroacoustics Testing
title The Update of an Aerodynamic Wind-Tunnel for Aeroacoustics Testing
spellingShingle The Update of an Aerodynamic Wind-Tunnel for Aeroacoustics Testing
Santana,Leandro Dantas
Aeroacoustic testing
Wind-tunnel noise
Wind-tunnel acoustic treatment
title_short The Update of an Aerodynamic Wind-Tunnel for Aeroacoustics Testing
title_full The Update of an Aerodynamic Wind-Tunnel for Aeroacoustics Testing
title_fullStr The Update of an Aerodynamic Wind-Tunnel for Aeroacoustics Testing
title_full_unstemmed The Update of an Aerodynamic Wind-Tunnel for Aeroacoustics Testing
title_sort The Update of an Aerodynamic Wind-Tunnel for Aeroacoustics Testing
author Santana,Leandro Dantas
author_facet Santana,Leandro Dantas
Carmo,Micael
Catalano,Fernando Martini
Medeiros,Marcello A. F.
author_role author
author2 Carmo,Micael
Catalano,Fernando Martini
Medeiros,Marcello A. F.
author2_role author
author
author
dc.contributor.author.fl_str_mv Santana,Leandro Dantas
Carmo,Micael
Catalano,Fernando Martini
Medeiros,Marcello A. F.
dc.subject.por.fl_str_mv Aeroacoustic testing
Wind-tunnel noise
Wind-tunnel acoustic treatment
topic Aeroacoustic testing
Wind-tunnel noise
Wind-tunnel acoustic treatment
description ABSTRACT: This paper describes the update and characterization of a previously pure aerodynamics wind-tunnel into a facility able to simultaneously execute aerodynamics and aeroacoustics testing. It is demonstrated that the application of high-performance acoustic materials on strategic positions of the wind-tunnel circuit and punctual actions can substantially reduce the background-noise level. This paper shows efficient measures which resulted to broadband-noise reduction of up to 5 dB and practically complete removal of spectral tones. In addition, it is demonstrated that the applied acoustic treatment reduced the turbulence level, measured at the test-section at maximum operational velocity, from the previous 0.25% level to 0.21%. As a minor penalty, the acoustic treatment reduced the flow velocity in 2% for the same electric-power input. Finally, the work described in this paper resulted on a wind-tunnel with good flow quality and capacity for aeroacoustics testing.
publishDate 2014
dc.date.none.fl_str_mv 2014-06-01
dc.type.driver.fl_str_mv info:eu-repo/semantics/article
dc.type.status.fl_str_mv info:eu-repo/semantics/publishedVersion
format article
status_str publishedVersion
dc.identifier.uri.fl_str_mv http://old.scielo.br/scielo.php?script=sci_arttext&pid=S2175-91462014000200111
url http://old.scielo.br/scielo.php?script=sci_arttext&pid=S2175-91462014000200111
dc.language.iso.fl_str_mv eng
language eng
dc.relation.none.fl_str_mv 10.5028/jatm.v6i2.308
dc.rights.driver.fl_str_mv info:eu-repo/semantics/openAccess
eu_rights_str_mv openAccess
dc.format.none.fl_str_mv text/html
dc.publisher.none.fl_str_mv Departamento de Ciência e Tecnologia Aeroespacial
publisher.none.fl_str_mv Departamento de Ciência e Tecnologia Aeroespacial
dc.source.none.fl_str_mv Journal of Aerospace Technology and Management v.6 n.2 2014
reponame:Journal of Aerospace Technology and Management (Online)
instname:Departamento de Ciência e Tecnologia Aeroespacial (DCTA)
instacron:DCTA
instname_str Departamento de Ciência e Tecnologia Aeroespacial (DCTA)
instacron_str DCTA
institution DCTA
reponame_str Journal of Aerospace Technology and Management (Online)
collection Journal of Aerospace Technology and Management (Online)
repository.name.fl_str_mv Journal of Aerospace Technology and Management (Online) - Departamento de Ciência e Tecnologia Aeroespacial (DCTA)
repository.mail.fl_str_mv ||secretary@jatm.com.br
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