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ロケットフェアリング模型の非定常PSP計測
https://jaxa.repo.nii.ac.jp/records/4406
https://jaxa.repo.nii.ac.jp/records/44061fa26430-f154-40f6-84bc-b4d003cc3a82
名前 / ファイル | ライセンス | アクション |
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65207034.pdf (1.1 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 | ロケットフェアリング模型の非定常PSP計測 | |||||
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_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 | Unsteady PSP measurement of a Rocket Fairing Model | |||||
著者 |
中北, 和之
× 中北, 和之× 今川, 健太郎× 高間, 良樹× 加藤, 裕之× 中島, 努× Nakakita, Kazuyuki× Imagawa, Kentaro× Takama, Yoshiki× Kato, Hiroyuki× Nakajima, Tsutomu |
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著者所属 | ||||||
宇宙航空研究開発機構 (JAXA) | ||||||
著者所属 | ||||||
宇宙航空研究開発機構 (JAXA) | ||||||
著者所属 | ||||||
宇宙航空研究開発機構 (JAXA) | ||||||
著者所属 | ||||||
宇宙航空研究開発機構 (JAXA) | ||||||
著者所属 | ||||||
宇宙航空研究開発機構 (JAXA) | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency (JAXA) | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency (JAXA) | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency (JAXA) | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency (JAXA) | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency (JAXA) | ||||||
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: 第43回流体力学講演会: 航空宇宙数値シミュレーション技術シンポジウム2011論文集 en : JAXA Special Publication: Proceedings of 43rd Fluid Dynamics Conference / Aerospace Numerical Simulation Symposium 2011 巻 JAXA-SP-11-015, p. 195-200, 発行日 2012-03-30 |
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会議概要(会議名, 開催地, 会期, 主催者等) | ||||||
内容記述タイプ | Other | |||||
内容記述 | 第43回流体力学講演会/航空宇宙数値シミュレーション技術シンポジウム2011 (2011年7月7日-8日. 早稲田大学国際会議場) 東京 | |||||
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 | 43rd Fluid Dynamics Conference / Aerospace Numerical Simulation Symposium 2011 (July 7-8, 2011. Waseda University, International Conference Center), Tokyo Japan | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | Unsteady Pressure-Sensitive Paint (PSP) measurement of a rocket fairing model was conducted at the JAXA 2m x 2m Transonic Wind Tunnel as a part of the campaign to investigate the steady and unsteady flow field around it and to obtain the CFD validation data. Anodized-aluminum PSP was coated on the model surface, and it was illuminated using a high-power blue laser diode. AA-PSP luminescence was measured by a high-speed camera, whose frame rate was 5kfps. The high-speed camera images were calculated to the Cp data using in-situ PSP calibration. Unsteady PSP data captured unsteady pressure data on the rocket fairing model as time-series Cp images. The unsteady phenomena on the model were significantly varied according to the Mach number and the angle of attack. Frequency analysis was also applied to the time-series Cp data. Unsteady pressure distribution was clearly investigated from the power spectrum results. | |||||
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: AA0065207034 | |||||
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-11-015 |