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完全航空機形状まわりの流れのナビエ・ストークスシミュレーション
https://jaxa.repo.nii.ac.jp/records/36777
https://jaxa.repo.nii.ac.jp/records/3677763863355-c93c-4233-900f-dc44d7bcefb1
名前 / ファイル | ライセンス | アクション |
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nalsp0030009.pdf (1.1 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 | 完全航空機形状まわりの流れのナビエ・ストークスシミュレーション | |||||
言語 | ||||||
言語 | jpn | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 流れ分布 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 完全航空機形状 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 格子点分配法 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 格子形成 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 並列ベクトル計算機 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 数値風洞 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 3次元Navier-Stokesシミュレーション | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | TVD風上法 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 有限体積法 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | マルチドメイン構造格子 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | Reynolds数 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 境界層 | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | flow distribution | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | complete aircraft configuration | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | point charge distribution method | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | grid generation | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | parallel vector computer | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | numerical wind tunnel | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | three dimensional Navier Stokes simulation | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | upwind scheme | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | finite volume method | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | multi domain structured grid | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Reynolds number | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | boundary layer | |||||
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 | Navier-Stokes simulation for a complete aircraft configuration | |||||
著者 |
高梨, 進
× 高梨, 進× 伊藤, 良三× 天野, 完一× 海田, 武司× Takanashi, Susumu× Ito, Ryozo× Amano, Kanichi× Kaiden, Takeshi |
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著者所属 | ||||||
航空宇宙技術研究所 | ||||||
著者所属 | ||||||
大興電子通信 | ||||||
著者所属 | ||||||
日本航空機開発協会 | ||||||
著者所属 | ||||||
三菱重工業 | ||||||
著者所属(英) | ||||||
en | ||||||
National Aerospace Laboratory | ||||||
著者所属(英) | ||||||
en | ||||||
Daiko Denshi Tsushin, Ltd | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aircraft Development Corporation | ||||||
著者所属(英) | ||||||
en | ||||||
Mitsubishi Heavy Industries, Ltd | ||||||
出版者 | ||||||
出版者 | 航空宇宙技術研究所 | |||||
出版者(英) | ||||||
出版者 | National Aerospace Laboratory (NAL) | |||||
書誌情報 |
航空宇宙技術研究所特別資料 en : Special Publication of National Aerospace Laboratory 巻 30, p. 47-52, 発行日 1996-01 |
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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 | 航空宇宙技術研究所 7-9 Jun. 1995 東京 日本 | |||||
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 | National Aerospace Laboratory 7-9 Jun. 1995 Tokyo Japan | |||||
抄録 | ||||||
内容記述タイプ | Abstract | |||||
内容記述 | 完全航空機形状周りの3次元Navier-Stokesシミュレーションを航空宇宙技術研究所の並列ベクトル計算機NWT(数値風洞)を用いて実行した。本システムの支配方程式は3次元Reynolds平均薄層Navier-Stokes方程式で、TVD風上法による有限体積法を用いて解いた。格子点分配法(point charge distribution method)を用いて、完全航空機形態周りのマルチドメイン構造格子による格子形成を行った。 | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | A three-dimensional Navier-Stokes simulation about a complete aircraft configuration has been carried out using the parallel vector computer called NWT (Numerical Wind Tunnel) at the National Aerospace Laboratory, Japan. The governing equations are three dimensional Reynolds-averaged thin-layer Navier-Stokes equations which are discretized by finite volume method with a TVD (Total Variable Diminishing) upwind scheme. The multidomain structured grid around the complete aircraft configuration has been generated by the point-charge distribution method. | |||||
ISSN | ||||||
収録物識別子タイプ | ISSN | |||||
収録物識別子 | 0289-260X | |||||
書誌レコードID | ||||||
収録物識別子タイプ | NCID | |||||
収録物識別子 | AN10097345 | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: AA0000294009 | |||||
レポート番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | レポート番号: NAL SP-30 |