JAXA Repository / AIREX 未来へ続く、宙(そら)への英知
64475002.pdf1.81 MB
titleJAXA0.8m×0.45m高Re数遷音速風洞におけるAGARD-B標準模型試験
Other TitleAGARD-B standard model tests in JAXA 0.8 m by 0.45 m high Reynolds number transonic wind tunnel
Author(jpn)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
Author(eng)Aoki, Yoshihisa; Kanda, Hiroshi; Sato, Mamoru; Nagai, Shinji; Itabashi, Yukihiro; Nishijima, Hironori; Kimura, Takeshi
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; IHIエアロスペース・エンジニアリング; IHIエアロスペース・エンジニアリング
Author Affiliation(eng)Japan Aerospace Exploration Agency (JAXA); Japan Aerospace Exploration Agency (JAXA); Japan Aerospace Exploration Agency (JAXA); Japan Aerospace Exploration Agency (JAXA); Japan Aero-Space Technology (JAST); IHI Aerospace Engineering (ISE); IHI Aerospace Engineering (ISE)
Issue Date2009-12-28
PublisherJapan Aerospace Exploration Agency (JAXA)
宇宙航空研究開発機構
Publication titleJAXA special publication: Proceedings of the Wind Technology Association 81st meeting
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
VolumeJAXA-SP-09-005
Publication date2009-12-28
Languagejpn
eng
AbstractAGARD-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.
DescriptionOriginal contains color illustrations
Wind Tunnel Technology Association Meeting
形態: カラー図版あり
会議情報: 第81回風洞研究会議(2008年11月20日-11月21日)
Document TypeConference Paper
JAXA Category特別資料
ISSN1349-113X
NCIDAA11984031
SHI-NOAA0064475002
Report NoJAXA-SP-09-005
URIhttps://repository.exst.jaxa.jp/dspace/handle/a-is/20666


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