Aoyama Gakuin University
Aoyama Gakuin University Graduate School
Japan Aerospace Exploration Agency Institute of Space and Astronautical Science
Japan Aerospace Exploration Agency Institute of Space and Astronautical Science
Japan Aerospace Exploration Agency Institute of Space and Astronautical Science
Japan Aerospace Exploration Agency Institute of Space and Astronautical Science
Aoyama Gakuin University
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）
Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA/ISAS)
雑誌名
宇宙航行の力学シンポジウム 平成16年度
雑誌名(英)
Symposium on Flight Mechanics and Astrodynamics 2004
ページ
124 - 127
発行年
2005-03
抄録（英）
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.
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
