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An experimental and numerical study on the compressible laminar flow control
https://jaxa.repo.nii.ac.jp/records/36829
https://jaxa.repo.nii.ac.jp/records/36829a2e6da82-c965-4015-bc3c-0e7d6bf5c544
名前 / ファイル | ライセンス | アクション |
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nalsp0031006.pdf (427.8 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 | ||||||
言語 | en | |||||
タイトル | An experimental and numerical study on the compressible laminar flow control | |||||
言語 | ||||||
言語 | eng | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 圧縮性層流制御 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 数値解析 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 境界層安定性 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 風洞試験 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 後退翼モデル | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 境界層遷移位置 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 境界層吸気 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 層流域 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 超音速層流制御 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 線形安定性理論 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 境界層安定解析コード | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 2次元境界層 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 擾乱 | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | compressible laminar flow control | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | numerical analysis | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | boundary layer stability | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | wind tunnel test | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | swept wing model | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | boundary layer transition location | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | boundary layer suction | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | laminar flow region | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | supersonic laminar flow control | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | linear stability theory | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | boundary layer stability analysis code | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | two dimensional boundary layer | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | disturbance | |||||
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 | ||||||
その他のタイトル | 圧縮性層流制御の実験的および数値的研究 | |||||
著者 |
吉田, 茂雄
× 吉田, 茂雄× 中野, 欣也× 塩沢, 信秋× Yoshida, Shigeo× Nakano, Kinya× Shiozawa, Nobuaki |
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著者所属 | ||||||
富士重工業 | ||||||
著者所属 | ||||||
富士重工業 | ||||||
著者所属 | ||||||
富士重工業 | ||||||
著者所属(英) | ||||||
en | ||||||
Fuji Heavy Industries, Ltd | ||||||
著者所属(英) | ||||||
en | ||||||
Fuji Heavy Industries, Ltd | ||||||
著者所属(英) | ||||||
en | ||||||
Fuji Heavy Industries, Ltd | ||||||
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 31, p. 81-90, 発行日 1996-05 |
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抄録 | ||||||
内容記述タイプ | Abstract | |||||
内容記述 | 境界層安定性について超音速風洞試験および数値解析を行った。風洞試験は後退翼モデルについて行った。境界層遷移位置をいくつかの迎え角で観測し、境界層吸気による層流域の拡大も観測した。その結果は超音速層流制御の妥当性を示した。線形安定性理論にもとづいて、境界層安定解析コードを開発し、その妥当性を2次元の境界層について確認した。風洞試験結果のひとつを解析し、擾乱の特性を明らかにした。 | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | Supersonic wind tunnel tests and numerical analyses were carried out on the boundary layer stability. Wind tunnel tests were performed on a swept wing model. Boundary layer transition locations were detected at various angles of attack and extensions of laminar flow regions by boundary layer suction were also observed. Consequently, the validity of supersonic laminar flow control was suggested. And a boundary layer stability analyses code was developed, based on the linear stability theory, and its validity was confirmed for two dimensional boundary layers. Then one of the wind tunnel test cases was analyzed, and characteristics of disturbances were clarified. | |||||
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: AA0000440006 | |||||
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-31 |