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の性能向上に関する一考察
Other TitleA Consideration for Scramjet Engine Performance Improvement
Author(jpn)佐藤, 茂; 福井, 正明; 渡邉, 孝宏; 宗像, 利彦
Author(eng)Sato, Shigeru; Fukui, Masaaki; Watanabe, Takahiro; Munakata, Toshihiko
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
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.
Issue Date2016-12-27
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48回流体力学講演会/第34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 48th Fluid Dynamics Conference / the 34th Aerospace Numerical Simulation Symposium
VolumeJAXA-SP-16-007
Start page125
End page129
Publication date2016-12-27
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 top 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. In the result of simulation by visualizing the stream lines in CFD, the effective stream lines are found useful for the fuel spreading. In this paper the authors describe results of trial combustion in two engine configurations including the improved configuration.
Description会議情報: 第48回流体力学講演会/第34回航空宇宙数値シミュレーション技術シンポジウム (2016年7月6日-8日. 金沢歌劇座), 金沢市, 石川
形態: カラー図版あり
Meeting Information: 48th Fluid Dynamics Conference /the 34th Aerospace Numerical Simulation Symposium (July 6-8, 2016. The Kanazawa Theatre), Kanazawa, Ishikawa, Japan
Physical characteristics: Original contains color illustrations
Document TypeConference Paper
JAXA Category特別資料
NASA Subject CategoryAircraft Propulsion and Power
ISSN1349-113X
NCIDAA11984031
SHI-NOAA1630031014
Report NoJAXA-SP-16-007
URIhttps://repository.exst.jaxa.jp/dspace/handle/a-is/577428


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