WEKO3
アイテム
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HB-2形状標準模型を用いたJAXA1.27m極超音速風洞3分力/空力加熱率測定試験
https://jaxa.repo.nii.ac.jp/records/6179
https://jaxa.repo.nii.ac.jp/records/6179dd78ed6e-daee-47d3-a933-67004511abb4
名前 / ファイル | ライセンス | アクション |
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49211008.pdf (945.3 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 | HB-2形状標準模型を用いたJAXA1.27m極超音速風洞3分力/空力加熱率測定試験 | |||||
言語 | ||||||
言語 | jpn | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 空力加熱 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 淀み圧力 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 淀み点エンタルピー | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 極超音速風洞 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 空力特性 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | マッハ数 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 熱伝達係数 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 不確実性分析 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | HB-2標準模型 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 偶然誤差 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 再現性 | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | aerodynamic heating | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | stagnation pressure | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | stagnation enthalpy | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | hypersonic wind tunnel | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | aerodynamic characteristic | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Mach number | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | heat transfer coefficient | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | uncertainty analysis | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | HB-2 standard model | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | random error | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | repeatability | |||||
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 | Force/heart flux measurements in the JAXA 1.27 m Hypersonic Wind-Tunnel using standard model HB-2 | |||||
著者 |
口石, 茂
× 口石, 茂× 渡辺, 重哉× 永井, 伸治× 津田, 尚一× 小山, 忠勇× 平林, 則明× 関根, 英夫× 穂積, 弘一× Kuchiishi, Shigeru× Watanabe, Shigeya× Nagai, Shinji× Tsuda, Shoichi× Koyama, Tadao× Hirabayashi, Noriaki× Sekine, Hideo× Hozumi, Koichi |
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著者所属 | ||||||
宇宙航空研究開発機構 総合技術研究本部 風洞技術開発センター | ||||||
著者所属 | ||||||
宇宙航空研究開発機構 総合技術研究本部 風洞技術開発センター | ||||||
著者所属 | ||||||
宇宙航空研究開発機構 総合技術研究本部 風洞技術開発センター | ||||||
著者所属 | ||||||
宇宙航空研究開発機構 総合技術研究本部 風洞技術開発センター | ||||||
著者所属 | ||||||
宇宙航空研究開発機構 総合技術研究本部 風洞技術開発センター | ||||||
著者所属 | ||||||
宇宙航空研究開発機構 総合技術研究本部 風洞技術開発センター | ||||||
著者所属 | ||||||
航空宇宙技術振興財団 | ||||||
著者所属 | ||||||
航空宇宙技術振興財団 | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency Wind Tunnel Technology Center, Institute of Aerospace Technology | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency Wind Tunnel Technology Center, Institute of Aerospace Technology | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency Wind Tunnel Technology Center, Institute of Aerospace Technology | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency Wind Tunnel Technology Center, Institute of Aerospace Technology | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency Wind Tunnel Technology Center, Institute of Aerospace Technology | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency Wind Tunnel Technology Center, Institute of Aerospace Technology | ||||||
著者所属(英) | ||||||
en | ||||||
Foundation for Promotion of Japanese Aerospace Technology | ||||||
著者所属(英) | ||||||
en | ||||||
Foundation for Promotion of Japanese Aerospace Technology | ||||||
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74回風洞研究会議論文集 en : JAXA Special Publication: Proceedings of the Wind Tunnel Technology Association 74th Meeting 巻 JAXA-SP-05-016, p. 48-52, 発行日 2006-02-28 |
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抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | In the present paper, results of force and heat flux measurement tests conducted in the JAXA 1.27 m Hypersonic Wind Tunnel (HWT) using the HB-2 standard model are presented. The tests were conducted at a nominal Mach number of 10, a stagnation enthalpy of 1 MJ/kg, and stagnation pressures from 1 to 6 MPa. Both for the force and heat tests, good data repeatability were confirmed. The heat transfer coefficient obtained from the IR thermography agreed well with the one from the thermocouple measurement. On the other hand, a conventional uncertainty estimation method which estimates the bias and random error components was applied to the force test data, whereas Monte Carlo approach was utilized to numerically estimate the uncertainty in the data reduction process of the heat flux data. The present experiment was conducted as a series of comparison test campaign between two hypersonic facilities in JAXA. The present test data is also expected to serve as a set of database for the validation of hypersonic computational fluid dynamics (CFD) codes. | |||||
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: AA0049211008 | |||||
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-05-016 |