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超音速三次元境界層の進行波モードの検出
https://jaxa.repo.nii.ac.jp/records/4274
https://jaxa.repo.nii.ac.jp/records/42749c5ab568-accb-4852-ade3-6d49badaf559
名前 / ファイル | ライセンス | アクション |
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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 | 超音速三次元境界層の進行波モードの検出 | |||||
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_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 | Observation of crossflow traveling mode in 3-D boundary layer on a yawed cylinder in Mach 2 flow | |||||
著者 |
高田, 晃輔
× 高田, 晃輔× 高木, 正平× 平田, 裕× 坂上, 昇史× Takada, Kosuke× Takagi, Shyohei× Hirata, Yutaka× Sakaue, Shyoji |
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著者所属 | ||||||
室蘭工業大学 | ||||||
著者所属 | ||||||
大阪府立大学 | ||||||
著者所属 | ||||||
大阪府立大学 | ||||||
著者所属 | ||||||
大阪府立大学 | ||||||
著者所属(英) | ||||||
en | ||||||
Muroran Institute of Technology | ||||||
著者所属(英) | ||||||
en | ||||||
Osaka Prefecture University | ||||||
著者所属(英) | ||||||
en | ||||||
Osaka Prefecture University | ||||||
著者所属(英) | ||||||
en | ||||||
Osaka Prefecture University | ||||||
出版者 | ||||||
出版者 | 宇宙航空研究開発機構(JAXA) | |||||
出版者(英) | ||||||
出版者 | Japan Aerospace Exploration Agency (JAXA) | |||||
書誌情報 |
宇宙航空研究開発機構特別資料 en : JAXA Special Publication: Proceedings of 44th Fluid Dynamics Conference / Aerospace Numerical Simulation Symposium 2012 巻 JAXA-SP-12-010, p. 203-206, 発行日 2013-03-29 |
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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 | 第44回流体力学講演会/航空宇宙数値シミュレーション技術シンポジウム2012 (2012年7月5日-6日. 富山国際会議場大手町フォーラム), 富山市, 富山県 | |||||
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 | 44th Fluid Dynamics Conference / Aerospace Numerical Simulation Symposium 2012 (July 5-6, 2012. Toyama International Conference Center), Toyama Japan | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | The present paper deals with instability and transition of 3-D boundary layer developing on a yawed circular cylinder with a sweepback of 60 degrees at Mach 2 in the supersonic wind tunnel of Muroran Institute of Technology. Visualized surface flow presents many striations regularly aligned almost to inviscid streamline, while hot-wire survey shows time-dependent broad-band disturbances, both of which originate from the so called cross-flow instability. It is found that comparison of experiments and stability analyses shows good agreement. The effect of condensation in the main flow on static pressure on a 5-degree semi-vertex cone model is discussed. | |||||
内容記述 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 形態: カラー図版あり | |||||
内容記述(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | Physical characteristics: Original contains color illustrations | |||||
ISSN | ||||||
収録物識別子タイプ | ISSN | |||||
収録物識別子 | 1349-113X | |||||
書誌レコードID | ||||||
収録物識別子タイプ | NCID | |||||
収録物識別子 | AA11984031 | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: AA0061958034 | |||||
レポート番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | レポート番号: JAXA-SP-12-010 |