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超音速領域におけるPIV 計測データの補正方法に関する研究: MTV データとの比較
https://jaxa.repo.nii.ac.jp/records/4016
https://jaxa.repo.nii.ac.jp/records/4016afe6ad90-e065-42a4-8173-6bcbbfb66232
名前 / ファイル | ライセンス | アクション |
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62268016.pdf (784.3 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 | ||||||
タイトル | 超音速領域におけるPIV 計測データの補正方法に関する研究: MTV データとの比較 | |||||
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 | Study on the Correction Method of PIV Data Measured in a Supersonic Region: Comparison with MTV Data | |||||
著者 |
三井, 克仁
× 三井, 克仁× 中野, 葵× 小池, 俊輔× 半田, 太郎× Mii, Katsuhito× Nakano, Aoi× Koike, Shunsuke× Handa, Taro |
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著者所属 | ||||||
九州大学 | ||||||
著者所属 | ||||||
三菱重工業株式会社 | ||||||
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 | ||||||
九州大学 | ||||||
著者所属(英) | ||||||
en | ||||||
Kyushu University | ||||||
著者所属(英) | ||||||
en | ||||||
Mitsubishi Heavy Industries, Ltd. | ||||||
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 | ||||||
Kyushu University | ||||||
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: 第45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2013論文集 en : JAXA Special Publication 巻 JAXA-SP-13-011, p. 89-94, 発行日 2014-03-31 |
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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45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2013 (2013年7月4日-5日. タワーホール船堀), 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 | 45th Fluid Dynamics Conference / Aerospace Numerical Simulation Symposium 2013 (July 4-5, 2013. Tower Hall Funabori), Tokyo, Japan | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | Particle image velocimetry (PIV) has become a powerful tool for the measurements of flow velocities in wind tunnel testing. However, it is generally difficult to apply the PIV to a supersonic flow because of unreliable particle traceability. In the present study, the method for correcting the PIV data measured in a supersonic flow is discussed. The tested flow is an underexpanded jet issuing from an orifice, the diameter of which is 6.0 mm. The jet has a region in which the gas is accelerated in a short distance (11 mm) from a sonic speed to a supersonic speed corresponding to Mach 3.7. The jet also has a normal shock wave called Mach disk across which the gas is decelerated rapidly from a supersonic speed to a subsonic speed. The PIV data is corrected by using the Basset-Boussinesq-Oseen (BBO) equation based on the assumption that the Stokes’ law is satisfied. The corrected PIV data is compared with the data measured by the molecular tagging velocimetry (MTV). The PIV data are reasonably improved in the entire measurement region. Especially, the corrected PIV data agree well with the MTV data downstream of the Mach disk. | |||||
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: AA0062268016 | |||||
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-13-011 |