| タイトル | Ceramic coating effect on liner metal temperatures of film-cooled annular combustor |
| 本文（外部サイト） | http://hdl.handle.net/2060/19790005927 |
| 著者（英） | Wear, J. D.; Liebert, C. H.; Claus, R. W. |
| 著者所属（英） | NASA Lewis Research Center |
| 発行日 | 1979-01-01 |
| 言語 | eng |
| 内容記述 | An experimental and analytical investigation was conducted to determine the effect of a ceramic coating on the average metal temperatures of full annular, film cooled combustion chamber liner. The investigation was conducted at pressures from 0.50 to 0.062. At all test conditions, experimental results indicate that application of a ceramic coating will result in significantly lower wall temperatures. In a simplified heat transfer analysis, agreement between experimental and calculated liner temperatures was achieved. Simulated spalling of a small portion of the ceramic coating resulted in only small increases in liner temperature because of the thermal conduction of heat from the hotter, uncoated liner metal. |
| NASA分類 | AIRCRAFT PROPULSION AND POWER |
| レポートNO | 79N14098
E-9732
NASA-TP-1323 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/176925 |
