@inproceedings{oai:jaxa.repo.nii.ac.jp:00004273,
 author = {金森, 正史 and 鈴木, 宏二郎 and Kanamori, Masashi and Suzuki, Kojiro},
 book = {宇宙航空研究開発機構特別資料, JAXA Special Publication: Proceedings of 44th Fluid Dynamics Conference / Aerospace Numerical Simulation Symposium 2012},
 month = {Mar},
 note = {第44回流体力学講演会/航空宇宙数値シミュレーション技術シンポジウム2012 (2012年7月5日-6日. 富山国際会議場大手町フォーラム), 富山市, 富山県, 44th Fluid Dynamics Conference / Aerospace Numerical Simulation Symposium 2012 (July 5-6, 2012. Toyama International Conference Center), Toyama Japan, In the past study, the author investigated a supersonic flow on a slow ascent and uncovered the existence of　two start points　of a shock wave in the flow field from a theoretical point of view. In this article, computational fluid dynamics (CFD) analyses are conducted on such flow field in order to investigate the existence from a practical view point. From the information of shockwaves, obtained from the shock detection algorithm with the compression wave exclusion filter, two start points can be certainly observed in the flow field. On the other hand, there are some differences between the theoretical and numerical result on the position of the start point. Such differences occur due to the effect of entropy, which is generated along the shock wave and is distributed downstream of the shock., 形態: カラー図版あり, Physical characteristics: Original contains color illustrations, 資料番号: AA0061958033, レポート番号: JAXA-SP-12-010},
 pages = {197--201},
 publisher = {宇宙航空研究開発機構(JAXA), Japan Aerospace Exploration Agency (JAXA)},
 title = {圧縮波領域中の衝撃波発生点に関する数値的考察},
 volume = {JAXA-SP-12-010},
 year = {2013}
}