| タイトル | Flame radiation and linear heat transfer in a tubular can combustor |
| 著者（英） | Humenik, F. M.; Claus, R. W.; Neely, G. M. |
| 著者所属（英） | NASA Lewis Research Center |
| 発行日 | 1984-01-01 |
| 言語 | eng |
| 内容記述 | Heat transfer within a combuster were examined. Total and spectral flame radiation in a tubular can combustor at a series of parameteric operating conditions was measured. Radiation measurements were taken for a range of inlet air pressures from 0.34 to 2.0 MPa, inlet air temperatures from 533 to 700 K, with two different fuels, Jet-A and ERBS. Measurements of linear temperatures combined with the parametric radiation results allowed a calculation of the combustor linear heat loads. Flame emissivity was determined from the spectral measurements. Previously announced in STAR as N84-13188 |
| NASA分類 | AIRCRAFT PROPULSION AND POWER |
| レポートNO | 84A21300
AIAA PAPER 84-0443 |
| 権利 | Copyright |
