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.
内容記述
形態: カラー図版あり
形態: CD-ROM1枚
内容記述（英）
Physical characteristics: Original contains color illustrations
Note: One CD-ROM
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
