@inproceedings{oai:jaxa.repo.nii.ac.jp:00003256,
 author = {豊永, 塁 and 山本, 姫子 and 溝渕, 泰寛 and 佐藤, 哲也 and Toyonaga, Rui and Yamamoto, Himeko and Mizobuchi, Yasuhiro and Sato, Tetsuya},
 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, 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., 形態: カラー図版あり, Physical characteristics: Original contains color illustrations, 資料番号: AA1730011022, レポート番号: JAXA-SP-17-004},
 pages = {143--146},
 publisher = {宇宙航空研究開発機構(JAXA), Japan Aerospace Exploration Agency (JAXA)},
 title = {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},
 volume = {JAXA-SP-17-004},
 year = {2017}
}