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0.5m極超音速風洞におけるマッハ5AGARD-B標準模型6分力試験
https://jaxa.repo.nii.ac.jp/records/5681
https://jaxa.repo.nii.ac.jp/records/5681af6a7e52-742b-4155-8bec-117e6f311857
名前 / ファイル | ライセンス | アクション |
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63607004.pdf (720.0 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 | ||||||
タイトル | 0.5m極超音速風洞におけるマッハ5AGARD-B標準模型6分力試験 | |||||
言語 | ||||||
言語 | jpn | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 研究施設 | |||||
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 | 風洞試験 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 風洞模型 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 流体力 | |||||
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 | 較正 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | AGARD-B | |||||
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 | シュリーレン写真法 | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | research facility | |||||
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 | wind tunnel test | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | wind tunnel model | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | aerodynamic force | |||||
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 | calibration | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | AGARD-B | |||||
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 | Schlieren photography | |||||
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 tests of an AGARD calibration model B in the JAXA 0.5 m Hypersonic Wind Tunnel at a nominal Mach number of 5 | |||||
著者 |
津田, 尚一
× 津田, 尚一× 小山, 忠勇× 平林, 則明× 渡利, 實× 関根, 英夫× 木伏, 淳子× 中村, 晃祥× Tsuda, Shoichi× Koyama, Tadao× Hirabayashi, Noriaki× Watari, Minoru× Sekine, Hideo× Kibushi, Junko× Nakamura, Akiyoshi |
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著者所属 | ||||||
宇宙航空研究開発機構 | ||||||
著者所属 | ||||||
宇宙航空研究開発機構 | ||||||
著者所属 | ||||||
宇宙航空研究開発機構 | ||||||
著者所属 | ||||||
宇宙航空研究開発機構 | ||||||
著者所属 | ||||||
航空宇宙技術振興財団 | ||||||
著者所属 | ||||||
スぺースサービス | ||||||
著者所属 | ||||||
航空宇宙技術振興財団 | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency | ||||||
著者所属(英) | ||||||
en | ||||||
Foundation for Promotion of Japanese Aerospace Technology | ||||||
著者所属(英) | ||||||
en | ||||||
Space Service | ||||||
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78回風洞研究会議論文集 en : JAXA Special Publication: Proceedings of the Wind Tunnel Technology Association 78th Meeting 巻 JAXA-SP-07-005, p. 33-39, 発行日 2007-08-31 |
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抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | Force tests were carried out using an AGARD-B calibration model in the JAXA 0.5 m Hypersonic Wind Tunnel (HWT1) at a nominal Mach number of 5. The aerodynamic characteristics of the AGARD-B calibration model were obtained successfully. The experimental results showed good agreement in comparison with those of other wind tunnels. The data obtained at the experiment and other tunnels were correlated well with the free stream Mach number. | |||||
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: AA0063607004 | |||||
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-07-005 |