@inproceedings{oai:jaxa.repo.nii.ac.jp:00016207,
 author = {高山, 明正 and 戸田, 諒 and 嶋田, 徹 and 北川, 幸樹 and Takayama, Akimasa and Toda, Ryo and Shimada, Toru and Kitagawa, Koki},
 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, In this study, to improve the regression rate and the combustion efficiency of hybrid rockets, swirling jets in the combustion chamber are multiplexed and parallelized. Swirling motion adds tangential velocity component to the flow and enhance the heat transfer to the grain. In addition to this, mixing around the central region of the chamber is expected to be enhanced by the interference of each swirling jet. Owing to these flow characteristics, the regression rate and the combustion efficiency will be improved. For the first step, the cold-flow visualizations have been done and the spatial distribution of flow directions has been obtained. From the results of the tests, it is suggested that mixing around the central region of the chamber is enhanced. However, each swirling jet disappeared and turned into a single swirl or axial flow at short distance from the exit of each swirler., 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: AA0061856071, レポート番号: STCP-2012-071},
 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 = {円管内における並列多重旋回流の可視化},
 year = {2013}
}