| タイトル | Summary of experimental heat-transfer results from the turbine hot section facility |
| 本文（外部サイト） | http://hdl.handle.net/2060/19930013870 |
| 著者（英） | Gladden, Herbert J.; Yeh, Fredrick C. |
| 著者所属（英） | NASA Lewis Research Center |
| 発行日 | 1993-04-01 |
| 言語 | eng |
| 内容記述 | Experimental data from the turbine Hot Section Facility are presented and discussed. These data include full-coverage film-cooled airfoil results as well as special instrumentation results obtained at simulated real engine conditions. Local measurements of airfoil wall temperature, airfoil gas-path static-pressure distribution, and local heat-transfer coefficient distributions are presented and discussed. In addition, measured gas and coolant temperatures and pressures are presented. These data are also compared with analyses from Euler and boundary-layer codes. |
| NASA分類 | FLUID MECHANICS AND HEAT TRANSFER |
| レポートNO | 93N23059
NASA-TP-3250
E-6615
NAS 1.60:3250 |
| 権利 | No Copyright |
