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title0.5m極超音速風洞におけるマッハ5AGARD-B標準模型6分力試験
Other TitleForce tests of an AGARD calibration model B in the JAXA 0.5 m Hypersonic Wind Tunnel at a nominal Mach number of 5
Author(jpn)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
Author(eng)Tsuda, Shoichi; Koyama, Tadao; Hirabayashi, Noriaki; Watari, Minoru; Sekine, Hideo; Kibushi, Junko; Nakamura, Akiyoshi
Author Affiliation(jpn)宇宙航空研究開発機構; 宇宙航空研究開発機構; 宇宙航空研究開発機構; 宇宙航空研究開発機構; 航空宇宙技術振興財団; スぺースサービス; 航空宇宙技術振興財団
Author Affiliation(eng)Japan Aerospace Exploration Agency; Japan Aerospace Exploration Agency; Japan Aerospace Exploration Agency; Japan Aerospace Exploration Agency; Foundation for Promotion of Japanese Aerospace Technology; Space Service; Foundation for Promotion of Japanese Aerospace Technology
Issue Date2007-08-31
PublisherJapan Aerospace Exploration Agency (JAXA)
宇宙航空研究開発機構
Publication title第78回風洞研究会議論文集
Proceedings of the Wind Tunnel Technology Association 78th Meeting
Start page33
End page39
Publication date2007-08-31
Languagejpn
AbstractForce 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.
DescriptionJAXA Special Publication
宇宙航空研究開発機構特別資料
Keywordsresearch facility; hypersonic wind tunnel; wind tunnel test; wind tunnel model; aerodynamic force; aerodynamic characteristic; calibration; AGARD-B; Mach number; Schlieren photography; 研究施設; 極超音速風洞; 風洞試験; 風洞模型; 流体力; 空力特性; 較正; AGARD-B; マッハ数; シュリーレン写真法
Document TypeConference Paper
JAXA Category特別資料
ISSN1349-113X
SHI-NOAA0063607004
Report NoJAXA-SP-07-005
URIhttps://repository.exst.jaxa.jp/dspace/handle/a-is/29288


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