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2次元翼模型加振装置の開発
https://jaxa.repo.nii.ac.jp/records/40627
https://jaxa.repo.nii.ac.jp/records/4062704fb5fee-c52e-4bfb-9d2b-4062b8b7bb84
名前 / ファイル | ライセンス | アクション |
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naltr0001403.pdf (1.4 MB)
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Item type | テクニカルレポート / Technical Report(1) | |||||
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公開日 | 2015-03-26 | |||||
タイトル | ||||||
タイトル | 2次元翼模型加振装置の開発 | |||||
言語 | ||||||
言語 | jpn | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 2次元翼 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 翼加振装置 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 振動翼 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 非定常流れ特性 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 流れの可視化 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | パーソナルコンピュータ制御 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 非定常空力特性 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 電動機駆動系 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 低速風洞 | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | two dimensional wing | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | wing oscillating system | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | oscillating wing | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | unsteady flow characteristic | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | flow visualization | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | personal computer control | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | unsteady aerodynamic characteristic | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | motor drive system | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | low wind tunnel | |||||
資源タイプ | ||||||
資源タイプ識別子 | http://purl.org/coar/resource_type/c_18gh | |||||
資源タイプ | technical report | |||||
その他のタイトル(英) | ||||||
その他のタイトル | Design and development of an oscillating system for 2-D wing models | |||||
著者 |
菊池, 孝男
× 菊池, 孝男× Kikuchi, Takao |
|||||
著者所属 | ||||||
航空宇宙技術研究所 構造研究部 | ||||||
著者所属(英) | ||||||
en | ||||||
National Aerospace Laboratory Structures Division | ||||||
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報告 en : Technical Report of National Aerospace Laboratory 巻 1403, p. 1-12, 発行日 2000-01 |
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抄録 | ||||||
内容記述タイプ | Abstract | |||||
内容記述 | 低速風洞で振動翼まわりの非定常流れ現象を調べるために斬新なデザインを行った2次元翼模型加振装置を開発した。本装置の特徴は、3台のモータをパソコンで制御することにより最大8Hzの擬似正弦波加振ができるとともに、翼模型の平均仰角、振動振幅、振動数を自動的に変更可能にしている点にある。 | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | To investigate the unsteady flow characteristics of the oscillating two-dimensional wing, an innovative mechanism to drive two-dimensional wing models was developed. The major design concepts of the system are: (1) quasi-harmonic pitching oscillation up to frequency of 8 Hz via three electric motors controlled by the personal computer; and (2) the mean-angles of attack, the amplitude and the frequencies can be changed automatically. The system is used for the flow visualization in a low wind tunnel to view the unsteady flow patterns around an oscillating two-dimensional wing model. | |||||
ISSN | ||||||
収録物識別子タイプ | ISSN | |||||
収録物識別子 | 0389-4010 | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: AA0001991000 | |||||
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 TR-1403 |