| タイトル | Summary of NASA aerodynamic and heat transfer studies in turbine vanes and blades |
| 著者（英） | Rohlik, H. E.; Stepka, F. S.; Moffitt, T. P. |
| 著者所属（英） | NASA Headquarters |
| 発行日 | 1976-11-01 |
| 言語 | eng |
| 内容記述 | Aerodynamic effects of trailing edge geometry, hole size, angle, spacing, and shape have been studied in two- and three-dimensional cascades and in a warm turbine test series. Heat transfer studies have been carried out in various two- and three-dimensional test facilities in order to provide corresponding heat transfer data. Results are shown in terms of cooling effectiveness and aerodynamic efficiency for various coolant fractions, coolant-primary temperature ratios, and cooling configurations. |
| NASA分類 | AIRCRAFT PROPULSION AND POWER |
| レポートNO | 77A28225
SAE PAPER 760917 |
| 権利 | Copyright |
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