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翼周り剥離流れ制御におけるシンセティックジェット駆動周波数と流れの不安定周波数の比較
https://jaxa.repo.nii.ac.jp/records/3635
https://jaxa.repo.nii.ac.jp/records/36352d8dee71-965a-4a2d-9c0c-ed59c8a76c2e
名前 / ファイル | ライセンス | アクション |
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AA1630005010.pdf (820.8 kB)
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Item type | 会議発表論文 / Conference Paper(1) | |||||
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公開日 | 2016-04-21 | |||||
タイトル | ||||||
タイトル | 翼周り剥離流れ制御におけるシンセティックジェット駆動周波数と流れの不安定周波数の比較 | |||||
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 | Flow instability and actuation frequency of a synthetic jet for separated flow control | |||||
著者 |
阿部, 圭晃
× 阿部, 圭晃× 野々村, 拓× 藤井, 孝藏× Abe, Yoshiaki× Nonomura, Taku× Fujii, Kozo |
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著者所属 | ||||||
東京大学 | ||||||
著者所属 | ||||||
宇宙航空研究開発機構宇宙科学研究所(JAXA) (ISAS) | ||||||
著者所属 | ||||||
宇宙航空研究開発機構宇宙科学研究所(JAXA) (ISAS) | ||||||
著者所属(英) | ||||||
en | ||||||
The University of Tokyo | ||||||
著者所属(英) | ||||||
en | ||||||
Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA) (ISAS) | ||||||
著者所属(英) | ||||||
en | ||||||
Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA) (ISAS) | ||||||
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: 第47回流体力学講演会/第33回航空宇宙数値シミュレーション技術シンポジウム論文集 en : JAXA Special Publication: Proceedings of the 47th Fluid Dynamics Conference / the 33rd Aerospace Numerical Simulation Symposium 巻 JAXA-SP-15-013, p. 73-78, 発行日 2016-03-08 |
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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47回流体力学講演会/第33回航空宇宙数値シミュレーション技術シンポジウム (2015年7月2日-3日. 東京大学生産技術研究所), 目黒区, 東京 | |||||
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 | 47th Fluid Dynamics Conference /the 33rd Aerospace Numerical Simulation Symposium (July 2-3, 2015. Institute of Industrial Science , the University of Tokyo), Meguro-ku, Tokyo, Japan | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | The large-eddy simulation (LES) of separation control using a synthetic jet is conducted around an NACA0015 airfoil of the chord Reynolds number 63,000. The linear stability analysis is together conducted to detect the unstable mode of the wall-normal fluctuation in the separation controlled flows. In the highly controlled cases, the harmonic modes of the input frequency directly enhances the KH instability modes which linearly develop in the separated shear layer. The other modes of both the higher and lower frequencies grow following the most unstable modes (the nonlinear growth regime), which effectively promotes the turbulent transition and the generation of large vortex structures. | |||||
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: AA1630005010 | |||||
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-15-013 |