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CFDワークショップ課題募集:CFDは翼型失速角を予測できるか?
https://jaxa.repo.nii.ac.jp/records/37438
https://jaxa.repo.nii.ac.jp/records/37438ff40c18b-9d15-4517-bac4-0bd4f6eb1c55
名前 / ファイル | ライセンス | アクション |
---|---|---|
nalsp0044005.pdf (403.7 kB)
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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 | CFDワークショップ課題募集:CFDは翼型失速角を予測できるか? | |||||
言語 | ||||||
言語 | jpn | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | CFD | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 数値流体力学 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 翼型 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 失速角予測 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 乱流モデル | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 2次元翼 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 格子形成法 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | アルゴリズム | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 設計点 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 2次元流 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 低速流れ | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 格子解像度 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 仰角 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 境界層特性分布図 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 空力特性図 | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | CFD | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | computational fluid dynamics | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | airfoil | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | stall angle prediction | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | turbulence model | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | two dimensional airfoil | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | grid generation method | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | algorithm | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | design point | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | two dimensional flow | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | low speed flow | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | grid resolution | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | angle of attack | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | bundary layer characteristic distribution diagram | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | aerodynamic characteristic diagram | |||||
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 | Call for papers, CFD workshop on 2D airfoil stall prediction: Can CFD predict airfoil stall angle? | |||||
著者 |
廣瀬, 直喜
× 廣瀬, 直喜× 中橋, 和博× 吉田, 憲司× 松尾, 裕一× 岩宮, 敏幸× Hirose, Naoki× Nakahashi, Kazuhiro× Yoshida, Kenji× Matsuo, Yuichi× Iwamiya, Toshiyuki |
|||||
著者所属 | ||||||
航空宇宙技術研究所 | ||||||
著者所属 | ||||||
東北大学 | ||||||
著者所属 | ||||||
航空宇宙技術研究所 | ||||||
著者所属 | ||||||
航空宇宙技術研究所 | ||||||
著者所属 | ||||||
航空宇宙技術研究所 | ||||||
著者所属(英) | ||||||
en | ||||||
National Aerospace Laboratory | ||||||
著者所属(英) | ||||||
en | ||||||
Tohoku University | ||||||
著者所属(英) | ||||||
en | ||||||
National Aerospace Laboratory | ||||||
著者所属(英) | ||||||
en | ||||||
National Aerospace Laboratory | ||||||
著者所属(英) | ||||||
en | ||||||
National Aerospace Laboratory | ||||||
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 44, p. 41-45, 発行日 1999-12 |
|||||
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 16-18 Jun. 1999 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 16-18 Jun. 1999 Tokyo Japan | |||||
抄録 | ||||||
内容記述タイプ | Abstract | |||||
内容記述 | 翼の失速特性と関連する大迎角流れ解析は多くが試みられ、すでに解決済みとの印象がある。しかし、定量的な信頼性については疑わしい。格子解像度、乱流モデル、計算アルゴリズムなどについて、精度のよい予測のために必要な知見を期待して、CFD(数値流体力学)ワークショップを計画し、以下の要項で課題募集を行った。(1)課題の目的は、CFDによる低速での翼型失速角の予測について、現状を把握し改善するための指針を明らかにすることである。(2)3種類の翼型を課題とする。(3)計算条件は、指定された迎角範囲を指定された角度刻みで、指定されたレイノルズ数とマッハ数について計算する。(4)流体力学方程式モデル、乱流モデル、および計算手法は、任意とする。その他、結果の提示、提出データファイル、応募締め切り、および問い合わせ先について示した。 | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | Many analyses of flow at high attack angles, relating to the stall characteristics of airfoils, have been attempted so far, and they give the impression that most of problems are already solved. But whether the problems of reliability were quantitatively solved is questionable. CFD (Computational Fluid Dynamics) workshop is planned to get the necessary knowledge of grid resolution, turbulence model and computational algorithm for the accurate prediction, and begins with an invitation of papers satisfying the following requirements. (1) The aim of the papers is to clarify the guideline to grasp and improve the present status in predictions of the airfoil stall angle at low speed using CFD. (2) The airfoil types are restricted to three. (3) The model of hydrodynamic equations, turbulence model and computational method are arbitrary. Moreover the presentation of results, the data file are to be submitted, the close of the subscription, and the reference is to be shown. | |||||
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: AA0001961005 | |||||
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-44 |