タイトル | Performance of a swirl-can combustor at idle conditions |
本文(外部サイト) | http://hdl.handle.net/2060/19720019318 |
著者(英) | Mularz, E. J.; Trout, A. M.; Niedzwiecki, R. W. |
著者所属(英) | NASA Lewis Research Center |
発行日 | 1972-06-01 |
言語 | eng |
内容記述 | Test results of a full annulus swirl-can combustor operated at simulated engine idle conditions indicated that significant improvements in combustion efficiency and accompanying reductions in pollutants could be realized with radial scheduling of fuel. Test conditions were an inlet air temperature of 478 K, a pressure of 4 atmospheres, and a reference velocity of 26 meters per second. At a fuel-air ratio of 0.008, radial scheduling of fuel increased combustion efficiency from less than 50 percent with no scheduling to nearly 100 percent and produced emission index values of unburned hydrocarbons and carbon monoxide of 10 and 40, respectively. |
NASA分類 | THERMODYNAMICS AND COMBUSTION |
レポートNO | 72N26968 NASA-TM-X-2578 E-6892 |
権利 | No Copyright |
URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/203135 |