@inproceedings{oai:jaxa.repo.nii.ac.jp:00013169,
 author = {菊池, 政雄 and 末松, 孝章 and 山本, 信 and 梅村, 章 and 小林, 秀昭 and 大上, 泰寛 and 野村, 浩司 and 三上, 真人 and 森上, 修 and 新城, 淳史 and 久, 康之 and Kikuchi, Masao and Suematsu, Takaaki and Yamamoto, Shin and Umemura, Akira and Kobayashi, Hideaki and Ogami, Yasuhiro and Nomura, Hiroshi and Mikami, Masato and Moriue, Osamu and Shinjo, Junji and Hisashi, Yasuyuki},
 book = {宇宙利用シンポジウム, Space Utilization Research: Proceedings of Space Utilization Symposium},
 month = {Feb},
 note = {第26回宇宙利用シンポジウム(2010年1月25日-26日, 宇宙航空研究開発機構宇宙科学研究本部相模原キャンパス), The Twenty-sixth Space Utilization Symposium (January 25-26, 2010: ISAS/JAXA Sagamihara, Japan), This paper describes activity report of Research Team(WG) on Combustion Dynamics of Fuel Droplets. In accordance with the objectives of this WG, ground-based microgravity experiments have been performed as well as numerical simulation. Also, preliminary planning of space experiment candidates has been performed to establish next space experiment, following previous 2 flight projects. Japan-Europe cooperative experiment "PHOENIX" employing TEXUS rocket, which was established as the first flight experiment from activity of this WG, was successfully performed by TEXUS#46 in November 2009. In addition, consideration on next-generation simulation technique for spray combustion has been discussed., 形態: カラー図版あり, 共催: 日本学術会議, 著者人数: 11人, Physical characteristics: Original contains color illustrations, joint hosting: The Science Council of Japan, 資料番号: AA0064730022},
 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)},
 title = {液滴群燃焼ダイナミクス研究チーム活動報告},
 volume = {26},
 year = {2010}
}