@inproceedings{oai:jaxa.repo.nii.ac.jp:00017456,
 author = {丹野, 英幸 and 伊藤, 勝宏 and 植田, 修一 and 小室, 智幸 and 佐藤, 和雄 and 小寺, 正敏 and Tanno, Hideyuki and Ito, Katsuhiro and Ueda, Shuichi and Komuro, Tomoyuki and Sato, Kazuo and Kodera, Masatoshi},
 book = {宇宙輸送シンポジウム　平成13年度, Proceedings of Space Transportation Symposium FY2001},
 month = {Apr},
 note = {Current status and future plan of scramjet research & development in the high enthalpy shock tunnel HIEST was described. The latest result of scramjet research performed in HIEST was reported, which result includes testing result of NAL sub-scale scramjet. The testing result was compared with that obtained in the blow down wind tunnel RJTF. Numerical analysis was also applied to understand flow in detail. Besides, a new scramjet design was also reported, which scramjet was planned to test under flow condition equivalent to flight Mach number 12. Moreover, flight test is planned which objective is to evaluate testing reliability of short test duration in HIEST., 資料番号: AA0033392028},
 pages = {111--114},
 publisher = {宇宙科学研究所, The Institute of Space and Astronautical Science (ISAS)},
 title = {高温衝撃風洞によるスクラムジェット開発の現状と計画},
 year = {2002}
}