| タイトル | Swirl-can combustor segment |
| 本文（外部サイト） | http://hdl.handle.net/2060/19700000310 |
| 著者（英） | Niedzwiecki, R.; Moyer, H.; Jones, R. |
| 発行日 | 1970-06-01 |
| 言語 | eng |
| 内容記述 | Combustor produces uniform circumferential and radial combustor exit temperature profiles and high combustion efficiency at high temperature loads. Absence of diluent air entry ports eliminates stress concentration points, low pressure fuel alleviates nozzle fouling, and abundant air at all burning stages reduces smoke. |
| NASA分類 | MACHINERY |
| レポートNO | 70B10322
LEW-11082 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/502071 |
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