@inproceedings{oai:jaxa.repo.nii.ac.jp:00016171,
 author = {高木, 翔平 and 富岡, 定毅 and 工藤, 賢司 and 村上, 淳郎 and 升谷, 五郎 and Takagi, Shohei and Tomioka, Sadatake and Kudo, Kenji and Murakami, Atsuo and Masuya, Goro},
 book = {平成24年度宇宙輸送シンポジウム: 講演集録, Proceedings of Space Transportation Symposium: FY2012},
 month = {Jan},
 note = {平成24年度宇宙輸送シンポジウム (2013年1月17日-1月18日. 宇宙航空研究開発機構宇宙科学研究所(JAXA)(ISAS)), 相模原市, 神奈川県, Space Transportation FY2012 (January 17-18, 2013. Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS)), Sagamihara, Kanagawa Japan, From the Mach 11 flight condition experiment result at HIEST, it was found that it was necessary to promote mixing to raise combustion efficiency. Therefore, the mixture state in the engine was investigated. The experiment conducted at supersonic wind tunnel. The mixture state was evaluated by gas sampling by the experiment without combustion. As a result, mixing promotion effect is match higher with the rocket side auxiliary injection than the cowl side auxiliary injection. Additionally, a mixture promotion effect by the incidence of the expansion wave to rocket exhaust was confirmed., 形態: カラー図版あり, 形態: PDF, Physical characteristics: Original contains color illustrations, Physical characteristics: PDF, 資料番号: AA0061856035, レポート番号: STCP-2012-035},
 pages = {1--8},
 publisher = {宇宙航空研究開発機構宇宙科学研究所(JAXA)(ISAS), Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS)},
 title = {RBCCエンジンのスクラムジェットモードでの流入空気とロケット排気との混合評価について},
 year = {2013}
}