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遷音速タービン翼間流れ三次元解析
https://jaxa.repo.nii.ac.jp/records/43154
https://jaxa.repo.nii.ac.jp/records/43154402a9782-94ef-43e0-8064-34312b080e20
名前 / ファイル | ライセンス | アクション |
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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 | 遷音速タービン翼間流れ三次元解析 | |||||
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 | Numerical Analysis of Fully Three-Dimensional Flow in Transonic Turbine Cascades | |||||
著者 |
小屋, 雅彦
× 小屋, 雅彦× 小竹, 進× Koya, Masahiko× Kotake, Susumu |
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著者所属 | ||||||
石川島播磨重工業株式会社 | ||||||
著者所属 | ||||||
東京大学工学部 | ||||||
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. 91-100, 発行日 1984-11 |
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抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | In order to calculate higher subsonic or transonic flows in highly three-dimensionally twisted turbine blade cascades, the finite volume integral method of solving the governing equations is implemented for the treatment of boundary conditions and the discretization scheme. The scheme developed here reduces the discretization error associated with the distorted grid configuration of highly three-dimensional blades. With the developed method, flows in three typical turbine blade cascades have been calculated. The present scheme can be applied to a fully three-dimensional flow through complete turbine stages. | |||||
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: NALSP0003012 | |||||
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 |