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A Study on Pressure Variation of a Rotor Blade Tip using PSP
https://jaxa.repo.nii.ac.jp/records/4141
https://jaxa.repo.nii.ac.jp/records/41419b563952-50f8-446b-8d40-58a3d643c708
名前 / ファイル | ライセンス | アクション |
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62070033.pdf (359.0 kB)
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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 | ||||||
言語 | en | |||||
タイトル | A Study on Pressure Variation of a Rotor Blade Tip using PSP | |||||
言語 | ||||||
言語 | eng | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | PSP | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | rotor blade | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | blade tip pressure | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | single-shot | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | lifetime | |||||
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 | |||||
著者 |
Kim, Kidong
× Kim, Kidong× Kwon, Kijung |
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著者所属 | ||||||
Aircraft System Engineering Department, University of Science and Technology (UST) | ||||||
著者所属 | ||||||
Aerodynamics Team, Korea Aerospace Research Institute (KARI) | ||||||
著者所属(英) | ||||||
en | ||||||
Aircraft System Engineering Department, University of Science and Technology (UST) | ||||||
著者所属(英) | ||||||
en | ||||||
Aerodynamics Team, Korea Aerospace Research Institute (KARI) | ||||||
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特別資料 en : JAXA Special Publication 巻 JAXA-SP-13-001E, p. 375-383, 発行日 2013-11-30 |
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会議概要(会議名, 開催地, 会期, 主催者等)(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | 5th Symposium on Integrating CFD and Experiments in Aerodynamics (October 3-5, 2012, Chofu Aerospace Center, Japan Aerospace Exploration Agency (JAXA)), Chofu, Tokyo, Japan | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | The present study was performed to verify the accuracy of measuring the upper surface pressure on a rotor blade tip using recently developed fast-response Pressure Sensitive Paint (PSP). Conventionally, in situ calibration was used to increase the accuracy of PSP measurement. However, it is very difficult to install the pressure measurement instruments such as a pressure tap on a rotor blade. Correction coefficient from CFD results was applied to this PSP experiment instead of in situ calibration. The experiment was performed using the small-scale rotor test stand in hovering condition. Blade had a NACA 0012 airfoil, and Rotational tip speed was about 87 m/s. Blade collective pitch was adjusted three different angle conditions (5 deg, 8 deg, 12 deg). The corrected PSP data was compared with well-known experimental pressure coefficients to examine the possibility of PSP application for pressure measurement on a rotor blade tip. | |||||
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 | 1349-113X | |||||
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: AA0062070033 | |||||
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-13-001E |