The Update of an Aerodynamic Wind-Tunnel for Aeroacoustics Testing
Autor(a) principal: | |
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Data de Publicação: | 2014 |
Outros Autores: | , , |
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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Journal of Aerospace Technology and Management (Online) |
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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 |
_version_ |
1754732530863439872 |