| タイトル | Parametric performance of a turbojet engine combustor using jet A and A diesel fuel |
| 本文（外部サイト） | http://hdl.handle.net/2060/19790011943 |
| 著者（英） | Butze, H. F.; Humenik, F. M. |
| 著者所属（英） | NASA Lewis Research Center |
| 発行日 | 1979-03-01 |
| 言語 | eng |
| 内容記述 | The performance of a single-can JT8D combustor was evaluated with Jet A and a high-aromatic diesel fuel over a parametric range of combustor-inlet conditions. Performance parameters investigated were combustion efficiency, emissions of CO, unburned hydrocarbons, and NOx, as well as liner temperatures and smoke. At all conditions the use of diesel fuel instead of Jet A resulted in increases in smoke numbers and liner temperatures; gaseous emissions, on the other hand, did not differ significantly between the two fuels. |
| NASA分類 | AIRCRAFT PROPULSION AND POWER |
| レポートNO | 79N20114
NASA-TM-79089
E-9913 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/176100 |
