JAXA Repository / AIREX 未来へ続く、宙(そら)への英知
titleJAXA 1m×1m 超音速風洞における2013年度気流検定試験結果
Other TitleWind Tunnel Calibration Test Result in JAXA 1m by 1m Supersonic Wind Tunnel in FY 2013
Author(jpn)青木, 良尚; 西島, 寛典; 安藤, 典久; 平野, 貴司; 渡辺, 光則; 満尾, 和徳
Author(eng)Aoki, Yoshihisa; Nishijima, Hironori; Ando, Norihisa; Hirano, Takashi; Watanabe, Mistunori; Mitsuo, Kazunori
Author Affiliation(jpn)宇宙航空研究開発機構(JAXA); 株式会社IHIエアロスペース・エンジニアリング(ISE); 株式会社IHIエアロスペース・エンジニアリング(ISE); 株式会社IHIエアロスペース・エンジニアリング(ISE); 宇宙航空研究開発機構(JAXA); 宇宙航空研究開発機構(JAXA)
Author Affiliation(eng)Japan Aerospace Exploration Agency (JAXA); IHI Aerospace Engineering Co. Ltd. (ISE); IHI Aerospace Engineering Co. Ltd. (ISE); IHI Aerospace Engineering Co. Ltd. (ISE); Japan Aerospace Exploration Agency (JAXA); Japan Aerospace Exploration Agency (JAXA)
Issue Date2015-03-25
Japan Aerospace Exploration Agency (JAXA)
Publication title宇宙航空研究開発機構特別資料: 第86-第90回風洞研究会議論文集
JAXA special publication: Proceedings of the Wind Tunnel Technology Association 86th-90th meeting
Start page64
End page67
Publication date2015-03-25
AbstractWe conducted annual wind tunnel calibration test on November in 2013 in JAXA 1m by 1m supersonic wind tunnel. Mach number distribution at test section and aerodynamic longitudinal forces of AGARD-B standard model were measured in this test campaign. Mach number distribution and aerodynamic longitudinal forces with roughness generally used in development test matched the past data. And we found the tendency of forebody axial force coefficient without roughness changed.
Description会議情報: 第90回風洞研究会議 (2014年5月22日-23日)
形態: カラー図版あり
Meeting Information: Wind Tunnel Technology Association 90th Meeting (May 22-23, 2014)
Physical characteristics: Original contains color illustrations
KeywordsCalibration Test; Mach Number Distribution; AGARD-B Standard Model
Document TypeConference Paper
JAXA Category特別資料
NASA Subject CategoryResearch and Support Facilities (Air)
Report NoJAXA-SP-14-011

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