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陽極酸化皮膜型感圧センサの非定常流への応用
https://jaxa.repo.nii.ac.jp/records/6559
https://jaxa.repo.nii.ac.jp/records/655903390933-9b0e-4a98-b079-fd98770e1028
名前 / ファイル | ライセンス | アクション |
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47776005.pdf (1.6 MB)
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Item type | 会議発表論文 / Conference Paper(1) | |||||
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公開日 | 2015-03-26 | |||||
タイトル | ||||||
タイトル | 陽極酸化皮膜型感圧センサの非定常流への応用 | |||||
言語 | ||||||
言語 | jpn | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 非定常空気力学 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 陽極酸化アルミニウム | |||||
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 | 振動流 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 小型液体振動子 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 吸着制御モデル | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | シュリーレン写真法 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 圧力分布 | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | unsteady aerodynamics | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | anodized aluminum | |||||
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 | oscillating flow | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | miniature fluidic oscillator | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | adsorption controlled model | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Schlieren photography | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | pressure distribution | |||||
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 | |||||
その他のタイトル(英) | ||||||
その他のタイトル | Anodized aluminum pressure sensitive paint for unsteady aerodynamic applications | |||||
著者 |
坂上, 博隆
× 坂上, 博隆× Sakaue, Hirotaka |
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著者所属 | ||||||
宇宙航空研究開発機構 | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency | ||||||
出版者 | ||||||
出版者 | 宇宙航空研究開発機構 | |||||
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特別資料: 境界層遷移の解明と制御研究会講演論文集 第33回・第34回 en : JAXA Special Publication: Proceedings of the 33rd and 34th JAXA Workshops on Investigation and Control of Boundary-Layer Transition 巻 JAXA-SP-04-002, p. 13-16, 発行日 2005-01-28 |
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抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | A miniature fluidic oscillator was used to demonstrate the capability of measuring oscillating unsteady aerodynamic fields with 6.4 kHz primary frequency. Pressure maps of various phases were captured by anodized aluminum pressure sensitive paint with platinum (II) meso-tetra (pentafluorolphenyl) porphine as a luminophore. Main uncertainty source comes from fitting the adsorption control model to calibration points and from the pulse width of illumination. The measurement uncertainty of the pressure was 4.65 percent. | |||||
ISSN | ||||||
収録物識別子タイプ | ISSN | |||||
収録物識別子 | 1349-113X | |||||
書誌レコードID | ||||||
収録物識別子タイプ | NCID | |||||
収録物識別子 | AA11984031 | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: AA0047776005 | |||||
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-SP-04-002 |