| タイトル | Antivortex Inlet Ribs for Fluid-Seals |
| 著者（英） | Jackson, E. D.; Chen, W. C.; Beatty, R. F. |
| 著者所属（英） | NASA Marshall Space Flight Center |
| 発行日 | 1984-04-01 |
| 言語 | eng |
| 内容記述 | Instability in rotating machinery reduced. Ring of ribs fastened to existing stator in turbopump pressure-seal inlet. Ribs suppress swirl in flow entering seal. Rib concept offers relatively inexpensive solution to some lateral-instability problems in many other systems with rotating pressure seals. |
| NASA分類 | MACHINERY |
| レポートNO | 83B10426
MFS-19793 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/408059 |
