| タイトル | Simulations of Flow Through the SSME LH2 Feed Line and LPFP Inducer |
| 本文（外部サイト） | http://hdl.handle.net/2060/20030066143 |
| 著者（英） | Dorney, Daniel J.; Rothermel, Jeffry |
| 著者所属（英） | NASA Marshall Space Flight Center |
| 発行日 | 2003-01-01 |
| 言語 | eng |
| 内容記述 | During a post-flight inspection of the liquid hydrogen feed lines leading the Space Shuttle main engines cracks were discover in slots on a flow liner just upstream of the low pressure fuel pump inducer. Numerical simulations have been performed for the feed line, the flow liner (including the slots and backing cavity) and the inducer. The predicted results have been compared with experimental data taken during hot-fire tests at NASA Stennis Space Center. |
| NASA分類 | Fluid Mechanics and Thermodynamics |
| 権利 | No Copyright |
