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  1. コンテンツタイプ
  2. 会議発表論文/会議発表用資料 (Conference Paper/Presentation)
  1. JAXA出版物(種類別)
  2. 特別資料 Special Publication(略称:SP)
  3. 2009年度
  4. JAXA-SP-09-014 「境界層遷移の解明と制御」研究会講演論文集(第43回・第44回)

低Re数の二次元翼から発生する空力音について: 数値手法

https://jaxa.repo.nii.ac.jp/records/4877
https://jaxa.repo.nii.ac.jp/records/4877
8cfd7d50-24d9-4819-be26-b430f2e932de
名前 / ファイル ライセンス アクション
64575001.pdf 64575001.pdf (660.1 kB)
Item type 会議発表論文 / Conference Paper(1)
公開日 2015-03-26
タイトル
タイトル 低Re数の二次元翼から発生する空力音について: 数値手法
言語
言語 jpn
キーワード
言語 en
主題Scheme Other
主題 trailing-edge noise, computational aeroacoustics, acoustic analogy
資源タイプ
資源タイプ識別子 http://purl.org/coar/resource_type/c_5794
資源タイプ conference paper
その他のタイトル(英)
その他のタイトル On the aerodynamic-noise generation from 2-D airfoils at low Reynolds numbers: Computational aspects
著者 池田, 友明

× 池田, 友明

WEKO 22238

池田, 友明

Search repository
高木, 正平

× 高木, 正平

WEKO 22239

高木, 正平

Search repository
Ikeda, Tomoaki

× Ikeda, Tomoaki

WEKO 22240

en Ikeda, Tomoaki

Search repository
Takagi, Shohei

× Takagi, Shohei

WEKO 22241

en Takagi, Shohei

Search repository
著者所属
宇宙航空研究開発機構研究開発本部
著者所属
宇宙航空研究開発機構研究開発本部
著者所属(英)
en
Aerospace Research and Development Directorate, Japan Aerospace Exploration Agency (JAXA)
著者所属(英)
en
Aerospace Research and Development Directorate, Japan Aerospace Exploration Agency (JAXA)
出版者
出版者 宇宙航空研究開発機構
出版者(英)
出版者 Japan Aerospace Exploration Agency (JAXA)
書誌情報 宇宙航空研究開発機構特別資料: 「境界層遷移の解明と制御」研究会講演論文集(第43回・第44回)
en : JAXA Special Publication: Proceedings of the 43rd and 44th JAXA Workshops on "Investigation and Control of Boundar-Layer Transition"

巻 JAXA-SP-09-014, 発行日 2010-02-26
会議概要(会議名, 開催地, 会期, 主催者等)
内容記述タイプ Other
内容記述 第43回(2008年10月2日-10月3日)「境界層遷移の解明と制御」研究会; 第44回(2009年3月26日-3月27日)「境界層遷移の解明と制御」研究会
会議概要(会議名, 開催地, 会期, 主催者等)(英)
内容記述タイプ Other
内容記述 43rd JAXA Workshops on "Investigation and Control of Boundar-Layer Transition" (October 2-3, 2008) ; 44th JAXA Workshops on "Investigation and Control of Boundar-Layer Transition" (March 26-27, 2009)
抄録(英)
内容記述タイプ Other
内容記述 Aerodynamic noise generated from 2-D airfoils is of interest in conjunction with the development of Karman-vortex shedding in the wake region. In this study, the computational aspects are discussed to reproduce the trailing-edge noise using acoustic analogies, based on the flow field obtained by a compressible flow solver with higher-order numerical schemes. The comparative study indicates that less-expensive acoustic analogies fail in representing the acoustically non-compact sound source with incompressible flow field However, by using a compressible near-field solution, the FW-H equation successfully predicts the far-field sound pressure directivity, for an accurate pressure fluctuation is provided at the airfoil surface.
内容記述
内容記述タイプ Other
内容記述 形態: カラー図版あり
内容記述(英)
内容記述タイプ Other
内容記述 Physical characteristics: Original contains color illustrations
ISSN
収録物識別子タイプ ISSN
収録物識別子 1349-113X
書誌レコードID
収録物識別子タイプ NCID
収録物識別子 AA11984031
資料番号
内容記述タイプ Other
内容記述 資料番号: AA0064575001
レポート番号
内容記述タイプ Other
内容記述 レポート番号: JAXA-SP-09-014
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