On closed-section wind-tunnel aeroacoustic experiments with a two-dimensional lifting body

Detalhes bibliográficos
Autor(a) principal: Amaral, Filipe Ramos do
Data de Publicação: 2019
Outros Autores: Pagani, Carlos do Carmo [UNESP], Himeno, Fernando Henrique Tadashi, Souza, Daniel Sampaio [UNESP], Medeiros, Marcello Augusto Faraco de
Tipo de documento: Artigo
Idioma: eng
Título da fonte: Repositório Institucional da UNESP
Texto Completo: http://dx.doi.org/10.1016/j.apacoust.2018.12.029
http://hdl.handle.net/11449/187265
Resumo: Slat noise experiments are sometimes performed to provide data for the validation of numerical procedures. Under such circumstances, closed-section wind-tunnels, in contrast with open-section ones, offer well-defined boundary conditions for simulations. Nevertheless, many difficulties arise in aeroacoustic experiments with two-dimensional lifting body tests in such wind-tunnels. Reverberation and acoustic images can also interfere with the measurements. This paper addresses the effects of the aforementioned issues on the MD30P30N airfoil slat aeroacoustic measurements. Conventional beamforming and DAMAS deconvolution techniques were employed for the acoustic data post-processing. Pressure taps were used in the assessment of spanwise and chordwise pressures on the high-lift airfoil model surfaces. The interaction between the airfoil and the wind-tunnel wall boundary-layer was mitigated by the application of suction on the tunnel wall and rendered a more two-dimensional flow. Acoustic polyurethane -based foam was applied on the test-section walls for reducing reverberation effects on the slat noise source maps. The results showed the error in the noise spectrum associated with the three-dimensional effect at the model ends may correspond to a decrement of 4 deg or higher of the entire wing angle of attack. The acoustic treatment over the wind-tunnel closed-section walls mitigated the mirror sources, nevertheless, the effects of such source images on both noise source maps and noise spectra in the region of interest were considered small.
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spelling On closed-section wind-tunnel aeroacoustic experiments with a two-dimensional lifting bodyAcoustic beamformingBoundary-layer suctionClosed-section wind-tunnelsDAMASSlat noiseWall acoustic treatmentSlat noise experiments are sometimes performed to provide data for the validation of numerical procedures. Under such circumstances, closed-section wind-tunnels, in contrast with open-section ones, offer well-defined boundary conditions for simulations. Nevertheless, many difficulties arise in aeroacoustic experiments with two-dimensional lifting body tests in such wind-tunnels. Reverberation and acoustic images can also interfere with the measurements. This paper addresses the effects of the aforementioned issues on the MD30P30N airfoil slat aeroacoustic measurements. Conventional beamforming and DAMAS deconvolution techniques were employed for the acoustic data post-processing. Pressure taps were used in the assessment of spanwise and chordwise pressures on the high-lift airfoil model surfaces. The interaction between the airfoil and the wind-tunnel wall boundary-layer was mitigated by the application of suction on the tunnel wall and rendered a more two-dimensional flow. Acoustic polyurethane -based foam was applied on the test-section walls for reducing reverberation effects on the slat noise source maps. The results showed the error in the noise spectrum associated with the three-dimensional effect at the model ends may correspond to a decrement of 4 deg or higher of the entire wing angle of attack. The acoustic treatment over the wind-tunnel closed-section walls mitigated the mirror sources, nevertheless, the effects of such source images on both noise source maps and noise spectra in the region of interest were considered small.Coordenação de Aperfeiçoamento de Pessoal de Nível Superior (CAPES)Conselho Nacional de Desenvolvimento Científico e Tecnológico (CNPq)Fundação de Amparo à Pesquisa do Estado de São Paulo (FAPESP)University of Sao Paulo (USP) Sao Carlos School of EngineeringSao Paulo State University (UNESP)Federal University of Sao Joao del-Rei (UFSJ)Sao Paulo State University (UNESP)CAPES: #00011/07-0CNPq: #141755/2012-1FAPESP: #2016/02970-5CNPq: #304859/2016-8Universidade de São Paulo (USP)Universidade Estadual Paulista (Unesp)Universidade Federal de Sergipe (UFS)Amaral, Filipe Ramos doPagani, Carlos do Carmo [UNESP]Himeno, Fernando Henrique TadashiSouza, Daniel Sampaio [UNESP]Medeiros, Marcello Augusto Faraco de2019-10-06T15:30:50Z2019-10-06T15:30:50Z2019-05-01info:eu-repo/semantics/publishedVersioninfo:eu-repo/semantics/article409-422http://dx.doi.org/10.1016/j.apacoust.2018.12.029Applied Acoustics, v. 148, p. 409-422.1872-910X0003-682Xhttp://hdl.handle.net/11449/18726510.1016/j.apacoust.2018.12.0292-s2.0-85059937139Scopusreponame:Repositório Institucional da UNESPinstname:Universidade Estadual Paulista (UNESP)instacron:UNESPengApplied Acousticsinfo:eu-repo/semantics/openAccess2021-10-22T18:13:05Zoai:repositorio.unesp.br:11449/187265Repositório InstitucionalPUBhttp://repositorio.unesp.br/oai/requestopendoar:29462021-10-22T18:13:05Repositório Institucional da UNESP - Universidade Estadual Paulista (UNESP)false
dc.title.none.fl_str_mv On closed-section wind-tunnel aeroacoustic experiments with a two-dimensional lifting body
title On closed-section wind-tunnel aeroacoustic experiments with a two-dimensional lifting body
spellingShingle On closed-section wind-tunnel aeroacoustic experiments with a two-dimensional lifting body
Amaral, Filipe Ramos do
Acoustic beamforming
Boundary-layer suction
Closed-section wind-tunnels
DAMAS
Slat noise
Wall acoustic treatment
title_short On closed-section wind-tunnel aeroacoustic experiments with a two-dimensional lifting body
title_full On closed-section wind-tunnel aeroacoustic experiments with a two-dimensional lifting body
title_fullStr On closed-section wind-tunnel aeroacoustic experiments with a two-dimensional lifting body
title_full_unstemmed On closed-section wind-tunnel aeroacoustic experiments with a two-dimensional lifting body
title_sort On closed-section wind-tunnel aeroacoustic experiments with a two-dimensional lifting body
author Amaral, Filipe Ramos do
author_facet Amaral, Filipe Ramos do
Pagani, Carlos do Carmo [UNESP]
Himeno, Fernando Henrique Tadashi
Souza, Daniel Sampaio [UNESP]
Medeiros, Marcello Augusto Faraco de
author_role author
author2 Pagani, Carlos do Carmo [UNESP]
Himeno, Fernando Henrique Tadashi
Souza, Daniel Sampaio [UNESP]
Medeiros, Marcello Augusto Faraco de
author2_role author
author
author
author
dc.contributor.none.fl_str_mv Universidade de São Paulo (USP)
Universidade Estadual Paulista (Unesp)
Universidade Federal de Sergipe (UFS)
dc.contributor.author.fl_str_mv Amaral, Filipe Ramos do
Pagani, Carlos do Carmo [UNESP]
Himeno, Fernando Henrique Tadashi
Souza, Daniel Sampaio [UNESP]
Medeiros, Marcello Augusto Faraco de
dc.subject.por.fl_str_mv Acoustic beamforming
Boundary-layer suction
Closed-section wind-tunnels
DAMAS
Slat noise
Wall acoustic treatment
topic Acoustic beamforming
Boundary-layer suction
Closed-section wind-tunnels
DAMAS
Slat noise
Wall acoustic treatment
description Slat noise experiments are sometimes performed to provide data for the validation of numerical procedures. Under such circumstances, closed-section wind-tunnels, in contrast with open-section ones, offer well-defined boundary conditions for simulations. Nevertheless, many difficulties arise in aeroacoustic experiments with two-dimensional lifting body tests in such wind-tunnels. Reverberation and acoustic images can also interfere with the measurements. This paper addresses the effects of the aforementioned issues on the MD30P30N airfoil slat aeroacoustic measurements. Conventional beamforming and DAMAS deconvolution techniques were employed for the acoustic data post-processing. Pressure taps were used in the assessment of spanwise and chordwise pressures on the high-lift airfoil model surfaces. The interaction between the airfoil and the wind-tunnel wall boundary-layer was mitigated by the application of suction on the tunnel wall and rendered a more two-dimensional flow. Acoustic polyurethane -based foam was applied on the test-section walls for reducing reverberation effects on the slat noise source maps. The results showed the error in the noise spectrum associated with the three-dimensional effect at the model ends may correspond to a decrement of 4 deg or higher of the entire wing angle of attack. The acoustic treatment over the wind-tunnel closed-section walls mitigated the mirror sources, nevertheless, the effects of such source images on both noise source maps and noise spectra in the region of interest were considered small.
publishDate 2019
dc.date.none.fl_str_mv 2019-10-06T15:30:50Z
2019-10-06T15:30:50Z
2019-05-01
dc.type.status.fl_str_mv info:eu-repo/semantics/publishedVersion
dc.type.driver.fl_str_mv info:eu-repo/semantics/article
format article
status_str publishedVersion
dc.identifier.uri.fl_str_mv http://dx.doi.org/10.1016/j.apacoust.2018.12.029
Applied Acoustics, v. 148, p. 409-422.
1872-910X
0003-682X
http://hdl.handle.net/11449/187265
10.1016/j.apacoust.2018.12.029
2-s2.0-85059937139
url http://dx.doi.org/10.1016/j.apacoust.2018.12.029
http://hdl.handle.net/11449/187265
identifier_str_mv Applied Acoustics, v. 148, p. 409-422.
1872-910X
0003-682X
10.1016/j.apacoust.2018.12.029
2-s2.0-85059937139
dc.language.iso.fl_str_mv eng
language eng
dc.relation.none.fl_str_mv Applied Acoustics
dc.rights.driver.fl_str_mv info:eu-repo/semantics/openAccess
eu_rights_str_mv openAccess
dc.format.none.fl_str_mv 409-422
dc.source.none.fl_str_mv Scopus
reponame:Repositório Institucional da UNESP
instname:Universidade Estadual Paulista (UNESP)
instacron:UNESP
instname_str Universidade Estadual Paulista (UNESP)
instacron_str UNESP
institution UNESP
reponame_str Repositório Institucional da UNESP
collection Repositório Institucional da UNESP
repository.name.fl_str_mv Repositório Institucional da UNESP - Universidade Estadual Paulista (UNESP)
repository.mail.fl_str_mv
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