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Design, construction and performance of a gust generating device for a half model test in the 6.5m×5.5m low speed wind tunnel.
https://jaxa.repo.nii.ac.jp/records/45188
https://jaxa.repo.nii.ac.jp/records/451880c2ad83c-47cb-4a9a-91d2-bf40f8c27bac
名前 / ファイル | ライセンス | アクション |
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naltr00929.pdf (2.6 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 | ||||||
言語 | en | |||||
タイトル | Design, construction and performance of a gust generating device for a half model test in the 6.5m×5.5m low speed wind tunnel. | |||||
言語 | ||||||
言語 | eng | |||||
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 | ||||||
その他のタイトル | 半截模型用突風発生装置の設計製作とその特性 | |||||
著者 |
鈴木, 誠三
× 鈴木, 誠三× 外立, 政隆× 室田, 勝一× 萱場, 重男× 菊池, 孝男× SUZUKI, Seizo× HASHIDATE, Masataka× MUROTA, Katsuichi× KAYABA, Shigeo× KIKUCHI, Takao |
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著者所属 | ||||||
航空宇宙技術研究所空気力学第二部 | ||||||
著者所属 | ||||||
航空宇宙技術研究所空気力学第二部 | ||||||
著者所属 | ||||||
航空宇宙技術研究所空気力学第二部 | ||||||
著者所属 | ||||||
航空宇宙技術研究所空気力学第二部 | ||||||
著者所属 | ||||||
航空宇宙技術研究所機体第一部 | ||||||
著者所属(英) | ||||||
en | ||||||
Second Aerodynamics Division, National Aerospace Laboratory(NAL) | ||||||
著者所属(英) | ||||||
en | ||||||
Second Aerodynamics Division, National Aerospace Laboratory(NAL) | ||||||
著者所属(英) | ||||||
en | ||||||
Second Aerodynamics Division, National Aerospace Laboratory(NAL) | ||||||
著者所属(英) | ||||||
en | ||||||
Second Aerodynamics Division, National Aerospace Laboratory(NAL) | ||||||
著者所属(英) | ||||||
en | ||||||
First Airframe Division, National Aerospace Laboratory(NAL) | ||||||
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 TR-929 巻 929, p. 38, 発行日 1987-04 |
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抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | A gust generating system was constructed for the test of a gust alleviation device conducted in the NAL′s 6.5m×5.5m low speed wind tennel. This system makes use of tip vortices shedding from a pair of cantileved, oscillating wings. The Dryden model of atmospheric turbulence was successfully simulated with this system; and wind tunnel tests for developing a gust load alleviation technique for an energy efficient type of future transport with a high aspect ratio wing were conducted with good results. | |||||
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: NALTR0929000 | |||||
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-929 |