@inproceedings{oai:jaxa.repo.nii.ac.jp:00016608,
 author = {江連, 諒介 and 坪井, 伸幸 and 林, 光一 and 山田, 英助 and Ezure, Ryosuke and Tsuboi, Nobuyuki and Hayashi, A. Koichi and Yamada, Eisuke and Tangirala, Venkat E.},
 book = {宇宙輸送シンポジウム: 講演集録, Proceedings of Space Transportation Symposium},
 month = {Jan},
 note = {平成21年度宇宙輸送シンポジウム(2010年1月14日-15日, 宇宙航空研究開発機構宇宙科学研究本部), Space Transportation Symposium (January 14-15, 2010. Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency(JAXA)),  Sagamihara, Kanagawa Japan, This paper presents effect of ambient flow for propulsive performance and the valve operations on H2/Air Pulse Detonation Engine using the system-level modeling, multi-cycle and automatic valve timing with detail chemical reaction model. The present results show that effect of ambient flow appears on the propulsive performance when the jet becomes highly over-expanded. However the flow doesn't influence the cycle time and the valve operations., 形態: カラー図版あり, 形態: CD-ROM1枚, Physical characteristics: Original contains color illustrations, Note: One CD-ROM, 資料番号: AA0064741038},
 publisher = {宇宙航空研究開発機構宇宙科学研究本部, Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)},
 title = {パルスデトネーションエンジンの推力性能推算に関する研究: 外部流の影響},
 volume = {平成21年度},
 year = {2010}
}