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埋め込み境界法を用いた機内空気流のLESの構築
https://jaxa.repo.nii.ac.jp/records/4929
https://jaxa.repo.nii.ac.jp/records/4929072ff637-ae7f-44f8-9911-792b7e434aa6
名前 / ファイル | ライセンス | アクション |
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64672031.pdf (1.5 MB)
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Item type | 会議発表論文 / Conference Paper(1) | |||||
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公開日 | 2015-03-26 | |||||
タイトル | ||||||
タイトル | 埋め込み境界法を用いた機内空気流のLESの構築 | |||||
言語 | ||||||
言語 | jpn | |||||
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 | Formation of LES of cabin air flow using immersed boundary method | |||||
著者 |
斎藤, 英文
× 斎藤, 英文× 梶島, 岳夫× Saito, Hidefumi× Kajishima, Takeo |
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著者所属 | ||||||
島津製作所航空機器事業部 | ||||||
著者所属 | ||||||
大阪大学大学院工学研究科 | ||||||
著者所属(英) | ||||||
en | ||||||
Aircraft Equipment Division, Shimadzu | ||||||
著者所属(英) | ||||||
en | ||||||
Graduate School of Engineering, Osaka University | ||||||
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: 第41回流体力学講演会/航空宇宙数値シミュレーション技術シンポジウム2009論文集 en : JAXA Special Publication: Proceedings fo 41st Fluid Dynamics Conference / Aerospace Numerical Simulation Symposium 2009 巻 JAXA-SP-09-011, 発行日 2010-02-26 |
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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 | 平成21年6月18-19日. 宇宙航空研究開発機構調布航空宇宙センター | |||||
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 | 18 June-19 June, 2009, Japan Aerospace Exploration Agency | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | We propose an analytical model as a process of understanding and improving cabin air in an aircraft. The model is based on Boeing 767 aircraft having two aisles in a wide body. In the model, interiors (i.e. ceilings, side wall, seats, and floor) and human bodies are taken into account. To deal with the complicated geometry of flow field efficiently, this model consists of Large Eddy Simulation (LES) based on Smagorinsky Model (SM) and is using IBM (Immersed Boundary Method) to adopt uniform staggered grids. The flow velocities at the immersed boundary cells are determined according to the volumetric fraction of solid. The effect of buoyancy is treated by Boussinesq approximation. The profiles of temperature and oxygen concentration are also calculated simultaneously. It is shown that the process is reproduced successfully for our purpose of optimizing cabin air quality. | |||||
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: AA0064672031 | |||||
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-09-011 |