| タイトル | Split-film anemometer measurements on an airfoil with turbulent separated flow |
| 著者（英） | Seetharam, H. C.; Wentz, W. H., Jr. |
| 著者所属（英） | Wichita State Univ.|Boeing Co. |
| 発行日 | 1979-01-01 |
| 言語 | eng |
| 内容記述 | Experimental studies of turbulent separation on airfoils have been conducted to aid in improving theoretical models of post-stall airfoil behavior. The studies utilize a variety of pressure and hot-film probes. The split-film anemometer has proved particularly valuable for measurement of highly turbulent reversing flows. Suggested techniques for on-line digital computer processing of the data are discussed. |
| NASA分類 | AERODYNAMICS |
| レポートNO | 79A42029 |
| 権利 | Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/426289 |
