WEKO3
アイテム
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タービン単段流れの数値シミュレーション
https://jaxa.repo.nii.ac.jp/records/36893
https://jaxa.repo.nii.ac.jp/records/368935817f57b-1e1b-4f3f-a02f-65b0cd2b3017
名前 / ファイル | ライセンス | アクション |
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nalsp0034034.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 | タービン単段流れの数値シミュレーション | |||||
言語 | ||||||
言語 | jpn | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 高圧タービン | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 単段流れ | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 静翼列 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 動翼列 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 3次元ナビエ・ストークスコード | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 非定常流れ解析コード | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | ブロック構造格子 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 非定常空力特性 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 圧力損失係数 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | ステージ全効率 | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | high pressure turbine | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | single stage flow | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | stator vane cascade | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | rotor blade cascade | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | three dimensional Navier Stokes code | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | unsteady flow analysis code | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | block structure grid | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | unsteady aerodynamic characteristic | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | pressure loss coefficient | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | stage total efficiency | |||||
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 | Unsteady single stage analysis for a high pressure turbine | |||||
著者 |
松永, 康二
× 松永, 康二× 竹内, 久雄× 平井, 健二× 松尾, 裕一× 菊地, 一雄× 野崎, 理× Matsunaga, Koji× Takeuchi, Hisao× Hirai, Kenji× Matsuo, Yuichi× Kikuchi, Kazuo× Nozaki, Osamu |
|||||
著者所属 | ||||||
石川島播磨重工業 | ||||||
著者所属 | ||||||
石川島播磨重工業 | ||||||
著者所属 | ||||||
石川島播磨重工業 | ||||||
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 | ||||||
Ishikawajima-Harima Heavy Industries Co Ltd | ||||||
著者所属(英) | ||||||
en | ||||||
Ishikawajima-Harima Heavy Industries Co Ltd | ||||||
著者所属(英) | ||||||
en | ||||||
Ishikawajima-Harima Heavy Industries Co 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 34, p. 189-194, 発行日 1997-01 |
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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 6-7 JUN. 1996 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 6-7 JUN. 1996 Tokyo Japan | |||||
抄録 | ||||||
内容記述タイプ | Abstract | |||||
内容記述 | 静翼列と動翼列からなる高圧タービン単段翼列配列を通る流れの数値シミュレーションを行った。単段翼列配列の非定常空力特性を評価するために、非定常アルゴリズム、ブロック構造格子システム、スライド格子手法を用いて3次元ナビエ・ストークスコードを開発し、検証計算を行った。ステージの空力性能を評価するために、静翼1翼間と回転する動翼2翼間を通る単純化した流れ場を同時に計算した。数値結果は、圧力損失係数、ステージ全効率などの実験データとかなりよく一致し、空力設計ツールとしての数値コードの有用性を立証した。 | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | The flows through a single stage high pressure turbine cascade configuration, consisting of a stator vane cascade and a rotor blade cascade, were numerically simulated. A 3-D Navier-Stokes code, using unsteady algorithm, block structure grid system and sliding grid technique, was developed and verified here to estimate the unsteady aerodynamic characteristics of the single stage cascade configuration. The simplified flowfield through one stator vane passage and moving two rotor blade passages were calculated simultaneously here to evaluate the aerodynamic performances of the stage. The numerical results showed a fairly good agreement with experimental data, such as pressure loss coefficients and stage total efficiencies, demonstrating the effectiveness of the numerical code as an aerodynamic design tool. | |||||
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: AA0000685034 | |||||
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-34 |