Conference Paper 圧縮性流体解析ソルバーFaSTAR を用いた超音速燃焼シミュレーション

豊永, 塁  ,  山本, 姫子  ,  溝渕, 泰寛  ,  佐藤, 哲也  ,  Toyonaga, Rui  ,  Yamamoto, Himeko  ,  Mizobuchi, Yasuhiro  ,  Sato, Tetsuya

In this study, the implementation of the combustion calculation code (flamelet approach) for a complex combustion field to a density-based fluid analysis solver, FaSTAR is conducted. With this calculation code, numerical exploration of non-reacting and reacting flow field of hydrogen fueled scramjet combustor is presented. The interaction between combustion and complex shock structures are well captured in the simulation.
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

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