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Dynamic Wind-Tunnel Testing of a Delta Wing Using a Multi-Degree-of-Freedom Robotic Manipulator
https://jaxa.repo.nii.ac.jp/records/4143
https://jaxa.repo.nii.ac.jp/records/4143ef5ee489-7304-4f3d-8b2a-1c3f9f84a086
名前 / ファイル | ライセンス | アクション |
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62070035.pdf (569.6 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 | Dynamic Wind-Tunnel Testing of a Delta Wing Using a Multi-Degree-of-Freedom Robotic Manipulator | |||||
言語 | ||||||
言語 | eng | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Dynamic Wind-Tunnel Testing | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Multi-Degree-of-Freedom | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Robotic Manipulator | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Delta Wing | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Vortex Breakdown | |||||
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 | |||||
著者 |
原, 達矢
× 原, 達矢× 沼田, 大樹× 浅井, 圭介× 伊藤, 崇文× 姜, 欣× Hara, Tatsuya× Numata, Daiju× Asai, Keisuke× Ito, Takafumi× Jiang, Xin |
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著者所属 | ||||||
東北大学大学院工学研究科 | ||||||
著者所属 | ||||||
東北大学大学院工学研究科 | ||||||
著者所属 | ||||||
東北大学大学院工学研究科 | ||||||
著者所属 | ||||||
東北大学大学院工学研究科 | ||||||
著者所属 | ||||||
東北大学大学院工学研究科 | ||||||
著者所属(英) | ||||||
en | ||||||
Graduate School of Engineering, Tohoku University | ||||||
著者所属(英) | ||||||
en | ||||||
Graduate School of Engineering, Tohoku University | ||||||
著者所属(英) | ||||||
en | ||||||
Graduate School of Engineering, Tohoku University | ||||||
著者所属(英) | ||||||
en | ||||||
Graduate School of Engineering, Tohoku University | ||||||
著者所属(英) | ||||||
en | ||||||
Graduate School of Engineering, Tohoku 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 巻 JAXA-SP-13-001E, p. 397-405, 発行日 2013-11-30 |
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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 | 5th Symposium on Integrating CFD and Experiments in Aerodynamics (October 3-5, 2012, Chofu Aerospace Center, Japan Aerospace Exploration Agency (JAXA)), Chofu, Tokyo, Japan | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | The purpose of this study is to measure the unsteady force acting on a slender delta wing in two degree-of-freedom (DoF) motion. A serial-type robot manipulator was used to oscillate the model in two modes; one is roll-yaw coupled lateral motion and the other is pitch-heave coupled longitudinal motion. Unsteady forces and moments were measured by a six-component balance and the effects of oscillation frequency and amplitude were evaluated. In the 2-DoF roll-yaw coupled mode, hysteresis loop was noted at high angles of attack and changes of rolling moment are delayed as compared with the 1-DoF case. In the pitch-heave coupled experiment, it was found that the effect of pitch rate on unsteady force is negligible at the frequency and amplitude ranges covered in this experiment. | |||||
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: AA0062070035 | |||||
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-13-001E |