@inproceedings{oai:jaxa.repo.nii.ac.jp:00003249,
 author = {佐藤, 茂 and 福井, 正明 and 宗像, 利彦 and 渡邉, 孝宏 and 髙橋, 正晴 and Sato, Shigeru and Fukui, Masaaki and Munakata, Toshihiko and Watanabe, Takahiro and Takahashi, Masaharu},
 book = {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},
 month = {Dec},
 note = {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, 49th Fluid Dynamics Conference /the 35th Aerospace Numerical Simulation Symposium (June 28-30, 2017. National Olympics Memorial Youth Center), Shibuya-ku, Tokyo, Japan, Japan 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., 形態: カラー図版あり, Physical characteristics: Original contains color illustrations, 資料番号: AA1730011015, レポート番号: JAXA-SP-17-004},
 pages = {105--110},
 publisher = {宇宙航空研究開発機構(JAXA), Japan Aerospace Exploration Agency (JAXA)},
 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},
 volume = {JAXA-SP-17-004},
 year = {2017}
}