| タイトル | Low Reynolds Number Nozzle Flow Study |
| 本文（外部サイト） | http://hdl.handle.net/2060/19870015993 |
| 著者（英） | Whalen, Margaret V. |
| 著者所属（英） | NASA Lewis Research Center |
| 発行日 | 1987-07-01 |
| 言語 | eng |
| 内容記述 | An experimental study of low Reynolds number nozzle flow was performed. A brief comparison was made between some of the experimental performance data and performance predicted by a viscous flow code. The performance of 15, 20, and 25 deg conical nozzles, bell nozzles, and trumpet nozzles was evaluated with unheated nitrogen and hydrogen. The numerical analysis was applied to the conical nozzles only, using an existing viscous flow code that was based on a slender-channel approximation. Although the trumpet and 25 deg conical nozzles had slightly better performance at lower Reynolds numbers, it is unclear which nozzle is superior as all fell within the experimental error band. The numerical rssults were found to agree with experimental results for nitrogen and for some of the hydrogen data. Some code modification is recommended to improve confidence in the performance prediction. |
| NASA分類 | SPACECRAFT PROPULSION AND POWER |
| レポートNO | 87N25426
NAS 1.15:100130
E-3679
NASA-TM-100130 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/149864 |
