| タイトル | Experimental studies of flow separation of three airfoils at low speeds |
| 本文（外部サイト） | http://hdl.handle.net/2060/19840020667 |
| 著者（英） | Wentz, W. H., Jr.; Seetharam, H. C.; Rodgers, E. J. |
| 著者所属（英） | Wichita State Univ. |
| 発行日 | 1982-03-01 |
| 言語 | eng |
| 内容記述 | Wind tunnel tests were conducted on the NASA LS(1)-0421 Mod, NACA 2412 and NASA GA(W)-2 airfoil sections at a Reynolds number of 2.2 x 10(6) and a Mach number of 0.13. Detailed measurements of flow fields associated with turbulent boundary layers of these airfoils were obtained at pre-stall, near-stall, and post-stall angles of attack. Velocity and pressure survey results over the airfoil and in the associated wake, are presented for fully attached flow conditions through the stalled flow condition. Extensive force, pressure, tuft survey, hot-film survey, local skin friction and boundary layer data are also included. |
| NASA分類 | AERODYNAMICS |
| レポートNO | 84N28736
NAS 1.26:3530
NASA-CR-3530
AR-79-2 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/158982 |
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