@inproceedings{oai:jaxa.repo.nii.ac.jp:00038828,
 author = {小島, 淳 and 高田, 仁志 and Kojima, Makoto and Takada, Satoshi},
 book = {日本航空宇宙学会北部支部2016年講演会ならびに第17回再使用型宇宙推進系シンポジウム, JSASS Northern Branch 2016 Annual Meeting and The 17th Symposiun on Propulsion System for Reusable Launch Vehicles},
 month = {Mar},
 note = {日本航空宇宙学会北部支部2016年講演会ならびに第17回再使用型宇宙推進系シンポジウム（2016年3月9日-10日. 北海道大学大学院工学研究院), 札幌市, 北海道, JAXA is considering apply a hydrostatic bearing for rocket engine turbopumps. As a first step, rotordynamic tests and numerical analysis were conducted to compare the results of each other. Because there was a difference in local pressure distribution and damping coefficient in each result, it became clear that it is necessary to continue performing improvements., 形態: カラー図版あり, 形態: CD-ROM1枚, Physical characteristics: Original contains color illustrations, Note: One CD-ROM, 資料番号: AC1600097000},
 publisher = {日本航空宇宙学会北部支部, Northern Branch of the Japan Society for Aeronautical and Space Sciences},
 title = {静圧軸受の静および動特性に関する研究: 数値解析の試行と試験結果について},
 volume = {17},
 year = {2016}
}