@inproceedings{oai:jaxa.repo.nii.ac.jp:00003491,
 author = {高橋, 政浩 and 高橋, 英美 and 冨田, 健夫 and Genin, Chloe and Schneider, Dirk and Takahashi, Masahiro and Takahashi, Hidemi and Tomita, Takeo and Genin, Chloe and Schneider, Dirk},
 book = {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},
 month = {Dec},
 note = {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, 48th Fluid Dynamics Conference /the 34th Aerospace Numerical Simulation Symposium (July 6-8, 2016. The Kanazawa Theatre), Kanazawa, Ishikawa, Japan, LOX/GCH4 combustion tests of sub-scaled dual-bell nozzle models have been conducted under research collaboration between DLR and JAXA. In this report, RANS simulation corresponding to these experiments was conducted to understand phenomena of the operation mode-transition and to evaluate prediction capability of the mode-transition condition in case with the combusting gas. The results showed that a turbulence model to be used has strong influence on the predicted mode-transition condition and that influence of an oxidizer-fuel mixture ratio on the mode-transition condition was different between CFD and the experiments., 形態: カラー図版あり, Physical characteristics: Original contains color illustrations, 資料番号: AA1630031016, レポート番号: JAXA-SP-16-007},
 pages = {137--140},
 publisher = {宇宙航空研究開発機構(JAXA), Japan Aerospace Exploration Agency (JAXA)},
 title = {デュアルベルノズル・サブスケール燃焼試験における作動点遷移予測について},
 volume = {JAXA-SP-16-007},
 year = {2016}
}