Table 4 Temperature-dependent heat transfer coefficient at the hot side of the copper liner (Kowollik 2015)
From: Stress evolution in thermal barrier coatings for rocket engine applications
Temperature / K | Heat transfer / Wm−2K−1 |
|---|---|
70 | 53779 |
167 | 55244 |
348 | 54881 |
562 | 52877 |
748 | 50754 |
873 | 49326 |
937 | 48637 |
962 | 48404 |
968 | 48354 |
969 | 48349 |
1031 | 47623 |
1138 | 46374 |
1259 | 45004 |
1361 | 43901 |
1427 | 43235 |
1461 | 42941 |
1474 | 42849 |
1477 | 42830 |
1478 | 42827 |