JAXA Repository / AIREX 未来へ続く、宙(そら)への英知
titleスクラムジェットエンジン性能向上に関する試み: 燃焼状態再現手法の検討
Other TitleA Trial for Scramjet Engine Performance Improvement: Preparing for Combustion Simulations
Author(jpn)佐藤, 茂; 福井, 正明; 宗像, 利彦; 渡邉, 孝宏; 髙橋, 正晴
Author(eng)Sato, Shigeru; Fukui, Masaaki; Munakata, Toshihiko; Watanabe, Takahiro; Takahashi, Masaharu
Author Affiliation(jpn)宇宙航空研究開発機構角田宇宙センター(JAXA)(KSPC); 株式会社スペースサービス; 株式会社日立ソリューションズ東日本; 株式会社日立ソリューションズ東日本; 株式会社日立ソリューションズ東日本
Author Affiliation(eng)Kakuda Space Center, Japan Aerospace Exploration Agency (JAXA)(KSPC); Space Service Co.,Ltd.; Hitachi Solutions East Japan,Ltd.; Hitachi Solutions East Japan,Ltd.; Hitachi Solutions East Japan,Ltd.
Issue Date2017-12-27
Publisher宇宙航空研究開発機構(JAXA)
Japan Aerospace Exploration Agency (JAXA)
Publication title宇宙航空研究開発機構特別資料: 第49回流体力学講演会/第35回航空宇宙数値シミュレーション技術シンポジウム論文集
JAXA Special Publication: Proceedings of the 49th Fluid Dynamics Conference / the 35th Aerospace Numerical Simulation Symposium
VolumeJAXA-SP-17-004
Start page105
End page110
Publication date2017-12-27
Languagejpn
eng
AbstractJapan Aerospace Exploration Agency has been investigating scramjet engines in Kakuda Space Center using RamJet Engine Test Facility (RJTF) et al. The engine tested at the flight condition of Mach 6 showed very steep fuel distribution. The fuel injected from the vertical injector on the side wall stays near the side wall and the tap wall along the engine. The steep fuel distribution is an obstacle for the engine performance completion. In order to solve the problem, the authors are focusing the influence of cowl shock wave on the fuel distribution and aerodynamic effects of strut. In this paper the authors describe results of trial combustion CFD in two engine configurations including the improved one.
Description会議情報: 第49回流体力学講演会/第35回航空宇宙数値シミュレーション技術シンポジウム (2017年6月28日-30日. 国立オリンピック記念青少年総合センター), 渋谷区, 東京
形態: カラー図版あり
Meeting Information: 49th Fluid Dynamics Conference /the 35th Aerospace Numerical Simulation Symposium (June 28-30, 2017. National Olympics Memorial Youth Center), Shibuya-ku, Tokyo, Japan
Physical characteristics: Original contains color illustrations
Document TypeConference Paper
JAXA Category特別資料
NASA Subject CategoryFluid Mechanics and Thermodynamics
ISSN(online)2433-2232
SHI-NOAA1730011015
Report NoJAXA-SP-17-004
URIhttps://repository.exst.jaxa.jp/dspace/handle/a-is/865299


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