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航技研6.5m×5.5m低速風洞におけるステレオPIVシステム開発予備試験
https://jaxa.repo.nii.ac.jp/records/6585
https://jaxa.repo.nii.ac.jp/records/658550e13df8-5876-4096-a757-36285c3952a4
名前 / ファイル | ライセンス | アクション |
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47429001.pdf (1.7 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 | 航技研6.5m×5.5m低速風洞におけるステレオPIVシステム開発予備試験 | |||||
言語 | ||||||
言語 | jpn | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 低速風洞 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 風洞試験 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 研究開発 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 粒子画像流速計測 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 粒子追跡流速測定 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | レーザドップラー流速計 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 流れの可視化 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 翼端渦 | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | low speed wind tunnel | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | wind tunnel test | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | research and development | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | particle image velocimetry | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | particle tracking velocimetry | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | laser doppler velocimeter | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | flow visualization | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | wing tip vortex | |||||
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 | Preliminary test of stereo PIV system applied to the 6.5 m x 5.5 m low speed wind tunnel | |||||
著者 |
加藤, 裕之
× 加藤, 裕之× 渡辺, 重哉× 星野, 秀雄× 末永, 尚史× 中谷, 輝臣× Kato, Hiroyuki× Watanabe, Shigeya× Hoshino, Hideo× Suenaga, Hisashi× Nakaya, Teruomi |
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著者所属 | ||||||
航空宇宙技術研究所 | ||||||
著者所属 | ||||||
航空宇宙技術研究所 | ||||||
著者所属 | ||||||
航空宇宙技術研究所 | ||||||
著者所属 | ||||||
航空宇宙技術研究所 | ||||||
著者所属 | ||||||
航空宇宙技術研究所 | ||||||
著者所属(英) | ||||||
en | ||||||
National Aerospace Laboratory | ||||||
著者所属(英) | ||||||
en | ||||||
National Aerospace Laboratory | ||||||
著者所属(英) | ||||||
en | ||||||
National Aerospace Laboratory | ||||||
著者所属(英) | ||||||
en | ||||||
National Aerospace Laboratory | ||||||
著者所属(英) | ||||||
en | ||||||
National Aerospace Laboratory | ||||||
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67回 風洞研究会議論文集 en : JAXA Special Publication: Proceedings of the Wind Tunnel Technology Association 67th Meeting 巻 JAXA-SP-03-004, p. 1-8, 発行日 2004-03-25 |
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抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | Preliminary tests of a stereo PIV system applied to a large-scale, low-speed wind tunnel are conducted. A tip vortex generated by a rectangular wing with an angle of attack and interfered flowfield between jet-engine exhaust and external flow are demonstratively measured by an off-the-shelf PIV system to examine the applicability of the stereo PIV technique to the large-scale wind tunnel and to acquire data required to determine the specifications of the system. The test results proved applicability of the stereo PIV to the large-scale, low-speed wind tunnel, while accuracy evaluation is to be done extensively in future. It was also found that the vibration of the wind tunnel has little effects on the velocity measurement accuracy while it does have effects on the location of the imaging area. | |||||
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: AA0047429001 | |||||
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-03-004 |