| タイトル | Boundary layer development on turbine airfoil suction surfaces |
| 著者（英） | Schlinker, R. H.; Sharma, O. P.; Bailey, D. A.; Wells, R. A. |
| 著者所属（英） | United Technologies Corp.|United Technologies Research Center |
| 発行日 | 1981-03-01 |
| 言語 | eng |
| 内容記述 | The results of a study supported by NASA under the Energy Efficient Engine Program, conducted to investigate the development of boundary layers under the influence of velocity distributions that simulate the suction sides of two state-of-the-art turbine airfoils, are presented. One velocity distribution represented a forward loaded airfoil ('squared-off' design), while the other represented an aft loaded airfoil ('aft loaded' design). These velocity distributions were simulated in a low-speed, high-aspect-ratio wind tunnel specifically designed for boundary layer investigations. It is intended that the detailed data presented in this paper be used to develop improved turbulence model suitable for application to turbine airfoil design. |
| NASA分類 | AERODYNAMICS |
| レポートNO | 81A30094
ASME PAPER 81-GT-204 |
| 権利 | Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/417110 |
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