@inproceedings{oai:jaxa.repo.nii.ac.jp:00013070,
 author = {野村, 浩司 and 相原, 秀紀 and 菊池, 政雄 and Nomura, Hiroshi and Aihara, Hideki and Kikuchi, Masao},
 book = {宇宙利用シンポジウム: 第27回: 平成22年度, Space Utilization Research, Vol. 27 2011: Proceedings of The Twenty-seventh Space Utilization Symposium},
 month = {Mar},
 note = {第27回宇宙利用シンポジウム (2011年1月24日-25日, 宇宙航空研究開発機構宇宙科学研究所相模原キャンパス), 相模原市, 神奈川県, The Twenty-seventh Space Utilization Symposium (January 24-25, 2011. Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS)), Sagamihara, Kanagawa Japan, Mono-dispersed fuel spray with narrow droplet diameter distribution (uniform spray) has been studied with several experimental apparatuses for microgravity. Spherical flame propagation was observed with the constant-pressure chamber and constant-volume chamber, and flame propagation speed and maximum burning pressure were measured with varying mean droplet diameter, total equivalence ratio, liquid equivalence ratio, gas equivalence ratio and pressure. Detailed observations of a flame stabilized in a uniform spray stream were performed with the uniform spray burners. The size of the uniform spray burner has been reduced to fit the combustion experimental module for ISS., 形態: カラー図版あり, Physical characteristics: Original contains color illustrations, 資料番号: AA0065129010},
 pages = {23--24},
 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 = {微小重力環境を利用した均一分散燃料噴霧の燃焼実験},
 volume = {27},
 year = {2011}
}