| タイトル | Parametric test results of a swirl-can combustor. |
| 著者（英） | Niedzwiecki, R. W.; Jones, R. E. |
| 発行日 | 1973-06-01 |
| 言語 | eng |
| 内容記述 | Pollutant levels of oxides of nitrogen, unburned hydrocarbons, and carbon monoxide were measured for three models of an experimental, annular swirl can combustor. The combustor was 1.067 meters in outer diameter, incorporated 120 modules, and was specifically designed for elevated exit temperature performance. Test conditions included combustor inlet temperatures of 589, 756, and 839 K, inlet pressures of 3 to 6.4 atmospheres, reference velocities of 21 to 38 meters per second, and combustor equivalence ratios, based on total combustor flows, of 0.206 to 1.028. Maximum oxides of nitrogen emission index values occurred at an equivalence ratio of 0.7 with lower values measured for both higher and lower equivalence ratios. |
| NASA分類 | PROPULSION SYSTEMS |
| レポートNO | 73A35471 |
| 権利 | Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/456867 |
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