WEKO3
アイテム
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感圧塗料を用いた宇宙研における大型風洞実験
https://jaxa.repo.nii.ac.jp/records/14652
https://jaxa.repo.nii.ac.jp/records/146526237f642-57a9-4909-b903-75377a80416b
Item type | 会議発表論文 / Conference Paper(1) | |||||
---|---|---|---|---|---|---|
公開日 | 2015-03-26 | |||||
タイトル | ||||||
タイトル | 感圧塗料を用いた宇宙研における大型風洞実験 | |||||
言語 | ||||||
言語 | jpn | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 風洞試験 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 感圧塗料 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 圧力測定 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | デルタ翼 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 風洞 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 超音速流 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 風洞模型 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 衝撃波 | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | wind tunnel test | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | pressure sensitive paint | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | pressure measurement | |||||
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 | wind tunnel | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | supersonic flow | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | wind tunnel model | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | shock wave | |||||
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 | |||||
アクセス権 | ||||||
アクセス権 | metadata only access | |||||
アクセス権URI | http://purl.org/coar/access_right/c_14cb | |||||
その他のタイトル(英) | ||||||
その他のタイトル | Pressure measurements with PSP in the JAXA/ISAS large-scale wind tunnel | |||||
著者 |
大内, 弘文
× 大内, 弘文× 藤井, 孝蔵× 佐藤, 清× 入門, 朋子× 林, 光一× Ouchi, Hirofumi× Fujii, Kozo× Sato, Kiyoshi× Irikado, Tomoko× Hayashi, Koichi |
|||||
著者所属 | ||||||
宇宙航空研究開発機構 宇宙科学研究本部 | ||||||
著者所属 | ||||||
宇宙航空研究開発機構 宇宙科学研究本部 | ||||||
著者所属 | ||||||
宇宙航空研究開発機構 宇宙科学研究本部 | ||||||
著者所属 | ||||||
宇宙航空研究開発機構 宇宙科学研究本部 | ||||||
著者所属 | ||||||
青山学院大学 | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency Institute of Space and Astronautical Science | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency Institute of Space and Astronautical Science | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency Institute of Space and Astronautical Science | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency Institute of Space and Astronautical Science | ||||||
著者所属(英) | ||||||
en | ||||||
Aoyama Gakuin University | ||||||
出版者 | ||||||
出版者 | 宇宙航空研究開発機構宇宙科学研究本部 | |||||
出版者(英) | ||||||
出版者 | Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA/ISAS) | |||||
書誌情報 |
宇宙航行の力学シンポジウム 平成15年度 en : Symposium on Flight Mechanics and Astrodynamics 2003 p. 25-28, 発行日 2004-05 |
|||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | Transonic flow fields over a delta wing and the shuttle model are investigated using PSP and TSP measurements (at the ISAS large-scaled wind tunnel). Since the models slightly move during wind-on, image registration is required for the acquisition of the accurate pressure distributions with the PSP in the large-scaled wind tunnel. An image registration method, which detects markers on the model surface automatically, used in the present study offers remarkable reduction of time for the image processing. As for the measurement for the delta wing, the automatic detection of markers is successfully performed and the pressure distributions obtained by PSP measurements agree well with the pressure tap data. The measurement for the shuttle model shows that difficulty still remains. | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: AA0047120007 |