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ルテニウム錯体系感圧塗料を用いた宇宙往還機模型の力計測
https://jaxa.repo.nii.ac.jp/records/14639
https://jaxa.repo.nii.ac.jp/records/14639de95d1d3-199e-4fa3-abc7-a406b4c4e01f
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 | ルテニウム錯体系感圧塗料を用いた宇宙往還機模型の力計測 | |||||
言語 | ||||||
言語 | jpn | |||||
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 | 再使用型宇宙機 | |||||
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 | ルテニウム錯体 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 遷・超音速風洞 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 画像処理 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 撮像技術 | |||||
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 | 風洞模型 | |||||
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 | reusable spacecraft | |||||
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 | ruthenium complex | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | transonic/supersonic wind tunnel | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | image processing | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | imaging technique | |||||
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 | wind tunnel model | |||||
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 | Force measurements of the shuttle model using PSP with Ruthenium(II) complex | |||||
著者 |
伊藤, 匡人
× 伊藤, 匡人× 大内, 弘文× 藤井, 孝蔵× 大山, 聖× 佐藤, 清× 入門, 朋子× 林, 光一× Ito, Masato× Ouchi, Hirofumi× Fujii, Kozo× Oyama, Akira× Sato, Kiyoshi× Irikado, Tomoko× Hayashi, Koichi A. |
|||||
著者所属 | ||||||
青山学院大学 | ||||||
著者所属 | ||||||
青山学院大学 大学院 | ||||||
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 | ||||||
Aoyama Gakuin University | ||||||
著者所属(英) | ||||||
en | ||||||
Aoyama Gakuin University Graduate School | ||||||
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16年度 en : Symposium on Flight Mechanics and Astrodynamics 2004 p. 124-127, 発行日 2005-03 |
|||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | Efficient and reliable PSP/TSP measurement system has been developed by using Ruthenium(II) complex and poly-IBM-co-TFEM binder and developing associated image data processing software SMAP for wind tunnel tests in small-scale to large-scale wind tunnels. The present PSP measurement system is inexpensive and easy-to-handle because it uses blue LED as light source. The optimal compounding ratio was found to obtain sufficient pressure and temperature sensitivity of PSP and TSP to improve its accuracy and reliability. SMAP is the GUI-based user-friendly free software that enables automated image data post-processing for PSP/TSP measurement. The present PSP/TSP measurement system has been validated by wind tunnel tests in the large-scale transonic/supersonic wind tunnel in ISAS/JAXA. As for wind tunnel tests of a Shuttle-Orbiter model, the image data post-processing has been successfully demonstrated by using image registration with edge detection and local marker detection. The lift force obtained using mapping process of the PSP measurement data generally agreed with the balance measurement data. | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: AA0048089032 |