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高レイノルズ数遷音速流翼型解析法の検証と実験との対応
https://jaxa.repo.nii.ac.jp/records/43171
https://jaxa.repo.nii.ac.jp/records/43171473b3757-f133-4c1b-883b-446efc08acac
名前 / ファイル | ライセンス | アクション |
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nalsp0003029.pdf (660.0 kB)
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Item type | テクニカルレポート / Technical Report(1) | |||||
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公開日 | 2015-03-26 | |||||
タイトル | ||||||
タイトル | 高レイノルズ数遷音速流翼型解析法の検証と実験との対応 | |||||
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_18gh | |||||
資源タイプ | technical report | |||||
その他のタイトル(英) | ||||||
その他のタイトル | Validation and Comparison with Experiment of a High Reynolds Number Transonic Flow Airfoil Analysis Code NSFOIL | |||||
著者 |
廣瀬, 直喜
× 廣瀬, 直喜× 河合, 伸坦× 小口, 慶子× 小寺, 智一× Hirose, Naoki× Kawai, Nobuhiro× Oguchi, Keiko× Kodera, Tomokazu |
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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 | ||||||
航空宇宙技術研究所研修生 | ||||||
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 | ||||||
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 SP-3 巻 3, p. 235-244, 発行日 1984-11 |
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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: NALSP0003029 | |||||
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-3 |