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超音速境界層:安定性と遷移予知
https://jaxa.repo.nii.ac.jp/records/37100
https://jaxa.repo.nii.ac.jp/records/37100f3fc6959-ca7d-41f8-89b8-28246b8a8f24
名前 / ファイル | ライセンス | アクション |
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nalsp0036010.pdf (268.1 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 | 超音速境界層:安定性と遷移予知 | |||||
言語 | ||||||
言語 | jpn | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 超音速境界層 | |||||
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 | 安定性解析 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 遷移予測 | |||||
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 | 後退角 | |||||
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 | 波束法 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 3次元擾乱 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 圧縮性境界層 | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | supersonic boundary layer | |||||
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 | stability analysis | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | transition prediction | |||||
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 | sweep angle | |||||
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 | wave packet method | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | three dimensional disturbance | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | compressible boundary layer | |||||
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 | An experimental and numerical study on supersonic boundary layer: Stability and transition prediction | |||||
著者 |
越岡, 康弘
× 越岡, 康弘× 谷, 泰寛× 吉田, 茂雄× Koshioka, Yasuhiro× Tani, Yasuhiro× Yoshida, Shigeo |
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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 36, p. 37-40, 発行日 1997-12 |
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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 26-28 Mar. 1997 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 26-28 Mar. 1997 Tokyo Japan | |||||
抄録 | ||||||
内容記述タイプ | Abstract | |||||
内容記述 | 超音速境界層安定性および遷移予測に関する風洞試験と安定性解析を行った。後退角が45度および65度の後退翼モデルについて風洞試験を行った。遷移現象を明らかにするために、境界層安定性解析コードを線形安定性理論および波束法に基づいて開発した。圧縮性境界層内の3次元擾乱の成長を解析により示した。 | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | Wind tunnel tests and stability analyzes were carried out on supersonic boundary layer stability and transition prediction. Wind tunnel tests were performed on a swept wing model, which has 45 and 65 degrees of sweep angle. To clarify transition phenomena, a boundary layer stability analysis code was developed based on the linear stability theory and wave packet method. The growth of three dimensional disturbance in the compressible boundary layer was shown by analyzes. | |||||
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: AA0001320010 | |||||
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-36 |