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衝撃風洞.新模型支持装置によるHB-2標準模型試験
https://jaxa.repo.nii.ac.jp/records/6125
https://jaxa.repo.nii.ac.jp/records/612580ece1bf-a144-42ec-9263-0c4135a66d71
名前 / ファイル | ライセンス | アクション |
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49495002.pdf (965.0 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 | 衝撃風洞.新模型支持装置によるHB-2標準模型試験 | |||||
言語 | ||||||
言語 | jpn | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 極超音速衝撃風洞 | |||||
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 | 模型支持装置 | |||||
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 | 振動測定 | |||||
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 | 風洞天秤 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 風洞試験 | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | hypersonic shock tunnel | |||||
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 | model support system | |||||
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 | vibration measurement | |||||
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 | wind tunnel balance | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | wind tunnel test | |||||
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 HB-2 standard model with a new model support system in the JAXA 0.44 m Hypersonic Shock Tunnel (HST) | |||||
著者 |
津田, 尚一
× 津田, 尚一× 渡利, 實× Tsuda, Shoichi× Watari, Minoru |
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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(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency | ||||||
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75回風洞研究会議論文集 en : JAXA Special Publication: Proceedings of the Wind Tunnel Technology Association 75th Meeting 巻 JAXA-SP-05-019, p. 17-21, 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 | Comprehensive HB-2 standard model tests are underway in the hypersonic wind tunnels in JAXA. The HB-2 force/moment test in Mach 10 flow was conducted in the 0.44 m Hypersonic Shock Tunnel (HST) with a new model support system. Vibration acceleration that is contaminated in the force/moment measurements was eliminated applying 'Oscillation identification technique'. The results of longitudinal characteristics were different from those obtained at the 1.27 m Hypersonic Wind Tunnel (HWT2). The sting bar of a new model support system seemed harmful. A significant improvement was observed when a wedge-type cover is attached to the bar. However, unsymmetrical feature still remains in the axial force. Detailed flow investigation with a new model support system is urgent. | |||||
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: AA0049495002 | |||||
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-05-019 |