@inproceedings{oai:jaxa.repo.nii.ac.jp:00013415,
 author = {大上, 泰寛 and 櫻井, 悟 and 長谷川, 翔一 and Jangi, Mehdi and 中村, 寿 and 吉永, 健太郎 and 小林, 秀昭 and Ogami, Yasuhiro and Sakurai, Satoru and Hasagawa, Shoichi and Jangi, Mehdi and Nakamura, Hisashi and Yoshinaga, Kentaro and Kobayashi, Hideaki},
 book = {宇宙利用シンポジウム　第24回　平成19年度, Space Utilization Research: Proceedings of the Twenty-fourth Space Utilization Symposium},
 month = {Mar},
 note = {To elucidate characteristics of a droplet flame as an elementary process of turbulent spray combustion, droplet combustion experiments in varying forced convection at high pressure were performed in microgravity. 1-butanole was used as a fuel and the maximum pressure was 0.4 MPa. High-speed back lit images of burning droplet were obtained and time history of the droplet diameter was measured using image processing. Results showed that maximum velocity in oscillating flow is predominant for the burning rate constant, meaning that the classical quasi-steady assumption is not valid. Mechanism of this droplet combustion characteristic was discussed based on the ratio of characteristic time scales of flow oscillation and gas diffusion., 資料番号: AA0063706039},
 pages = {166--169},
 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/ISAS)},
 title = {微小重力環境を利用した高圧下における液滴火炎の流速変動への応答に関する研究},
 year = {2008}
}