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翼端間隙を有するタービン翼列流れの検証
https://jaxa.repo.nii.ac.jp/records/37843
https://jaxa.repo.nii.ac.jp/records/3784341c4f30c-d86e-40a5-9f34-e216e7c36764
名前 / ファイル | ライセンス | アクション |
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nalsp0027006.pdf (558.6 kB)
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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 | 翼端間隙を有するタービン翼列流れの検証 | |||||
言語 | ||||||
言語 | jpn | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | タービン翼列 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 翼列流れ | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 内部流れ | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | タービン段解析 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 翼端隙間 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 流れ数値シミュレーション | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | CFDコード検証 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | CFD対風洞相関 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 全圧損失 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | エンジン空気力学 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 超音速輸送機 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | TVDスキーム | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 動翼 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 温度分布 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 圧力分布 | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | turbine cascade | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | cascade flow | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | internal flow | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | turbine stage analysis | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | tip clearance | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | numerical flow simulation | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | CFD code verification | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | CFD wind tunnel correlation | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | total pressure loss | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | engine aerodynamics | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | supersonic transport airplane | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | TVD scheme | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | rotor distribution | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | temperature distribution | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | stator | |||||
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 | Verification of turbine cascade flow with tip clearance | |||||
著者 |
清水, 邦弘
× 清水, 邦弘× 三宅, 慶明× 野崎, 理× 菊地, 一雄× 田村, 敦宏× Shimizu, Kunihiro× Miyake, Yoshiaki× Nozaki, Osamu× Kikuchi, Kazuo× Tamura, Atsuhiro |
|||||
著者所属 | ||||||
三菱重工業 | ||||||
著者所属 | ||||||
三菱重工業 | ||||||
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 | ||||||
Mitsubishi Heavy Industries Ltd | ||||||
著者所属(英) | ||||||
en | ||||||
Mitsubishi Heavy Industries Ltd | ||||||
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 27, p. 75-80, 発行日 1994-12 |
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抄録 | ||||||
内容記述タイプ | Abstract | |||||
内容記述 | 本論文は翼端間隙をもつ単段タービン翼列の検証結果を示す。タービン翼列内の流れは、航空宇宙技術研究所によって開発された、Chakravarthy-OsherのTVDスキームに基く段解析コードCAS3DMを用いて計算された。結果は、静翼の全圧損失および動翼の全圧と全温の分布につき実験データとよく一致し、翼列の損失を推定するための設計手段としてコードが有用であることを示す。 | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | This paper presents verification results of a single stage turbine cascade with tip clearance. The flow through turbine cascades is calculated by using stage analysis code (Cascade three dimensional (CAS3DM)) based on Chakravarthy-Osher's TVD (Total Variation Diminishing) scheme developed by National Aerospace Laboratory. The results show good agreements with the experimental data on the total pressure loss of the stator and the total pressure and total temperature distributions of the rotor, indicating the effectiveness of the code as a design tool for estimating loss of the cascade. | |||||
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: AA0004174006 | |||||
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-27 |