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JAXA 感圧塗料(PSP)計測システムの研究開発(1): 概要編
https://jaxa.repo.nii.ac.jp/records/1976
https://jaxa.repo.nii.ac.jp/records/1976ef167862-6454-46ea-87f7-90abfe67dced
名前 / ファイル | ライセンス | アクション |
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62264000.pdf (14.5 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 | JAXA 感圧塗料(PSP)計測システムの研究開発(1): 概要編 | |||||
言語 | ||||||
言語 | jpn | |||||
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 | Research and Development of JAXA Pressure-Sensitive Paint (PSP) Measurement System (I) | |||||
著者 |
満尾, 和徳
× 満尾, 和徳× 中北, 和之× 栗田, 充× 渡辺, 重哉× Mitsuo, Kazunori× Nakakita, Kazuyuki× Kurita, Mitsuru× Watanabe, Shigeya |
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著者所属 | ||||||
宇宙航空研究開発機構航空本部風洞技術開発センター(JAXA) | ||||||
著者所属 | ||||||
宇宙航空研究開発機構航空本部風洞技術開発センター(JAXA) | ||||||
著者所属 | ||||||
宇宙航空研究開発機構航空本部風洞技術開発センター(JAXA) | ||||||
著者所属 | ||||||
宇宙航空研究開発機構航空本部風洞技術開発センター(JAXA) | ||||||
著者所属(英) | ||||||
en | ||||||
Wind Tunnel Technology Center, Institute of Aeronautical Technology, Japan Aerospace Exploration Agency (JAXA) | ||||||
著者所属(英) | ||||||
en | ||||||
Wind Tunnel Technology Center, Institute of Aeronautical Technology, Japan Aerospace Exploration Agency (JAXA) | ||||||
著者所属(英) | ||||||
en | ||||||
Wind Tunnel Technology Center, Institute of Aeronautical Technology, Japan Aerospace Exploration Agency (JAXA) | ||||||
著者所属(英) | ||||||
en | ||||||
Wind Tunnel Technology Center, Institute of Aeronautical Technology, Japan Aerospace Exploration Agency (JAXA) | ||||||
出版者 | ||||||
出版者 | 宇宙航空研究開発機構(JAXA) | |||||
出版者(英) | ||||||
出版者 | Japan Aerospace Exploration Agency (JAXA) | |||||
書誌情報 |
宇宙航空研究開発機構研究開発報告 en : JAXA Research and Development Report 巻 JAXA-RR-13-005, p. 1-42, 発行日 2014-02-28 |
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抄録 | ||||||
内容記述タイプ | Abstract | |||||
内容記述 | 感圧塗料(Pressure-sensitive paint:PSP)と呼ばれる発光強度が圧力によって変化する塗料を用いた表面圧力場計測が注目されている.これまでの電子式センサーによる離散的な点計測とは異なり,面で圧力場を計測することができる.風洞技術開発センターでは大型風洞群へPSP 計測システムを適用するための実用化研究を進めてきた.感圧塗料,光学系,および画像処理を含む全計測システムの開発を独自で行っている.本レポートでは,風洞技術開発センターが開発したPSP 計測技術の概要を示すとともに,試験結果の一部を紹介する. | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | Pressure-field measurement technique using Pressure-Sensitive Paint (PSP) has been developed for acquiring global pressure images on wind tunnel models. PSP makes use of the sensitivity of the luminescent materials to the air pressure. PSP measurement technique provides a simple and an inexpensive way to obtain full-field pressure image on aerodynamic model surface with high spatial resolution. JAXA has developed the PSP measurement system for practical use in Wind Tunnel Technology Center (WINTEC). In this paper, the summary of the JAXA PSP measurement technique in industrial wind tunnels were reported. | |||||
内容記述 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 形態: カラー図版あり | |||||
内容記述(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | Physical characteristics: Original contains color illustrations | |||||
ISSN | ||||||
収録物識別子タイプ | ISSN | |||||
収録物識別子 | 1349-1113 | |||||
書誌レコードID | ||||||
収録物識別子タイプ | NCID | |||||
収録物識別子 | AA1192675X | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: AA0062264000 | |||||
レポート番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | レポート番号: JAXA-RR-13-005 |