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JAXA0.8m×0.45m高Re数遷音速風洞におけるAGARD-B標準模型試験
https://jaxa.repo.nii.ac.jp/records/5154
https://jaxa.repo.nii.ac.jp/records/51549b54e5cb-d18f-48fd-bbf4-a9bfadf0fad1
名前 / ファイル | ライセンス | アクション |
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64475002.pdf (1.9 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 | JAXA0.8m×0.45m高Re数遷音速風洞におけるAGARD-B標準模型試験 | |||||
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 | AGARD-B standard model tests in JAXA 0.8 m by 0.45 m high Reynolds number transonic wind tunnel | |||||
著者 |
青木, 良尚
× 青木, 良尚× 神田, 宏× 佐藤, 衛× 永井, 伸治× 板橋, 幸広× 西島, 寛典× 木村, 毅× Aoki, Yoshihisa× Kanda, Hiroshi× Sato, Mamoru× Nagai, Shinji× Itabashi, Yukihiro× Nishijima, Hironori× Kimura, Takeshi |
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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 | ||||||
IHIエアロスペース・エンジニアリング | ||||||
著者所属 | ||||||
IHIエアロスペース・エンジニアリング | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency (JAXA) | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency (JAXA) | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency (JAXA) | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency (JAXA) | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aero-Space Technology (JAST) | ||||||
著者所属(英) | ||||||
en | ||||||
IHI Aerospace Engineering (ISE) | ||||||
著者所属(英) | ||||||
en | ||||||
IHI Aerospace Engineering (ISE) | ||||||
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81回風洞研究会議論文集 en : JAXA Special Publication: Proceedings of the Wind Technology Association 81st meeting 巻 JAXA-SP-09-005, 発行日 2009-12-28 |
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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81回風洞研究会議(2008年11月20日-11月21日) | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | AGARD-B full and semi-span standard model tests were conducted in JAXA 0.8 m by 0.45 m high Reynolds number transonic wind tunnel. The semi-span model was tested either on the reflection plate or on the peniche. All the data were corrreced by a panel method about the wall interference effects. The full-span model data agreed well with the AGARDograph 64 data. And the semi-span model on the reflection plate agreed with the full-span data more than those on the peniche. However, the drag data of the semi-span model showed large differences to those of the full-span model. | |||||
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 | |||||
内容記述(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | Wind Tunnel Technology Association Meeting | |||||
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: AA0064475002 | |||||
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-09-005 |