| Área de identificação | |
| Tipo de Referência | Artigo em Evento (Conference Proceedings) |
| Site | mtc-m21b.sid.inpe.br |
| Código do Detentor | isadg {BR SPINPE} ibi 8JMKD3MGPCW/3DT298S |
| Identificador | 8JMKD3MGP5W34M/3FA44S9 |
| Repositório | sid.inpe.br/mtc-m21b/2013/11.26.16.48.07 |
| Última Atualização | 2018:08.27.12.45.29 marcelo.pazos@inpe.br |
| Metadados | sid.inpe.br/mtc-m21b/2013/11.26.16.48.08 |
| Última Atualização dos Metadados | 2018:08.27.12.45.30 marcelo.pazos@inpe.br |
| ISBN | 9781624102134 |
| Rótulo | scopus 2013-11 |
| Chave de Citação | RedonnetCunhKhel:2013:NuSiLa |
| Título | Numerical simulation of landing gear noise via weakly coupled CFD-CAA calculations  |
| Ano | 2013 |
| Data de Acesso | 24 fev. 2021 |
| Número de Arquivos | 1 |
| Tamanho | 2310 KiB |
| Área de contextualização | |
| Autor | 1 Redonnet, S. 2 Cunha, Guilherme 3 Khelil, S. B. |
| Grupo | 1 2 LCP-CTE-INPE-MCTI-GOV-BR |
| Afiliação | 1 ONERA (French Aerospace Centre), CFD and Aeroacoustics Department, BP 72 - 29 av Division Leclerc, Châtillon, 92322, France 2 Instituto Nacional de Pesquisas Espaciais (INPE) 3 ONERA (French Aerospace Centre), Applied Aerodynamic Department, BP 72 - 29 av Division Leclerc, Châtillon, 92322, France |
| Endereço de e-Mail | marcelo.pazos@inpe.br |
| Nome do Evento | AIAA/CEAS Aeroacoustics Conference, 19. |
| Localização do Evento | Berlin |
| Data | 27 -29 May 2013 |
| Páginas | 66 |
| Título do Livro | Proceedings |
| Cidade da Editora | Berlin |
| Tipo Secundário | PRE CI |
| Histórico | 2014-01-09 13:37:31 :: administrator -> marcelo.pazos@sid.inpe.br :: 2013 2014-01-10 11:07:36 :: marcelo.pazos@sid.inpe.br -> administrator :: 2013 2018-06-04 03:14:09 :: administrator -> marcelo.pazos@inpe.br :: 2013 |
| Área de conteúdo e estrutura | |
| É a matriz ou uma cópia? | é a matriz |
| Estágio do Conteúdo | concluido |
| Transferível | 1 |
| Tipo do Conteudo | External Contribution |
| Tipo de Versão | publisher |
| Palavras-Chave | Coupled calculation, Coupling procedure, Landing gear noise, Nose landing gear, Numerical predictions, Reference solution, Refraction effects, Unsteady aerodynamics, Acoustic noise, Aeroacoustics, Aerodynamic configurations, Landing gear (aircraft), Noise pollution, Computational fluid dynamics. |
| Resumo | The present work is relevant from the numerical prediction of aircraft noise via aeroacoustics hybrid methods. It is part of a more extensive effort, which final objective is the development of a robust and accurate CFD-CAA weak coupling methodology. Within this framework, we focus here on the so-called surface coupling approach, a technique that allows conducting weakly coupled CFD-CAA calculations. Such approach (which had been previously developed and validated on simpler cases) is here applied to a ralistic problem of aircraft noise, given by the acoustic emission of a nose landing gear in approach flight (a configuration that was addressed in the Airbus LAGooN program). For doing so, several preliminary tasks are first addressed, which are carefully handled and thoroughly detailed. Two CFD-CAA coupled calculations are then conducted, both being based on i) a same CFD dataset coming from an unsteady aerodynamic calculation (zonal DES), and ii) two distinct CAA calculations of different characteristics; first, a CFD-CAA calculation is conducted for the so-called 'baseline' configuration (i.e. isolated gear within a free-field flow), so as to validate the coupling procedure, as well as to generate a reference solution for subsequent assessment of the mean flow effects induced by the experimental set-up. The validation of the coupling procedure is conducted via a direct comparison of the CFD-CAA results with either experimental or numerical (CFD, CFD-FWH) outputs obtained in the near-, mid, and/or far-field. With the view of assessing the mean flow effects, an alternative CFD-CAA calculation is then performed, which incorporates the realistic sheared jet flow characterizing the anechoic facility. This allows assessing the (partial) convection and refraction effects induced by such jet mean flow, which helps underscoring better the relevance of the present CFD-CAA hybrid approach when it comes to handle real-life noise problems. |
| Area | COMB |
| Arranjo | |
| Conteúdo da Pasta source | não têm arquivos |
| Conteúdo da Pasta agreement | não têm arquivos |
| Área de condições de acesso e uso | |
| URL dos dados | http://urlib.net/rep/8JMKD3MGP5W34M/3FA44S9 |
| URL dos dados zipados | http://urlib.net/zip/8JMKD3MGP5W34M/3FA44S9 |
| Idioma | en |
| Grupo de Usuários | administrator marcelo.pazos@inpe.br |
| Grupo de Leitores | administrator marcelo.pazos@inpe.br |
| Visibilidade | shown |
| Permissão de Atualização | não transferida |
| Área de fontes relacionadas | |
| Repositório Espelho | iconet.com.br/banon/2006/11.26.21.31 |
| Unidades Imediatamente Superiores | 8JMKD3MGPCW/3ET38CH |
| Acervo Hospedeiro | sid.inpe.br/mtc-m21b/2013/09.26.14.25.20 |
| Área de notas | |
| Campos Vazios | accessionnumber archivingpolicy archivist callnumber copyholder copyright creatorhistory descriptionlevel dissemination doi edition editor electronicmailaddress format issn lineage mark nextedition notes numberofvolumes orcid organization parameterlist parentrepositories previousedition previouslowerunit progress project publisher readpermission resumeid rightsholder secondarydate secondarykey secondarymark serieseditor session shorttitle sponsor subject targetfile tertiarymark tertiarytype type url volume |
