| タイトル | Experimental studies of the separated flow over a NASA GA(W)-1 airfoil |
| 著者（英） | Goradia, S.; Mehta, J. M. |
| 著者所属（英） | Illinois Inst. of Tech. |
| 発行日 | 1984-04-01 |
| 言語 | eng |
| 内容記述 | The separated flow over the 17-percent-thick blunt-trailing-edge NASA GA(W)-1 airfoil is investigated experimentally at angles of attack 10.3-18.4 deg and velocities up to 92 m/sec in the 1.09 x 0.76 x 1.22-m working section of a closed-circuit wind tunnel, with typical Reynolds numbers of the order 4 x 10 to the 6th. The results are presented graphically and characterized. Separated-flow velocity profiles and skin-friction distributions are obtained, and the boundary-layer integral properties are shown to be in good agreement with the separation criteria of Sandborn and Kline (1961). The chordwise development of the mean velocity is reduced to a universal curve, and some similarity is found in the outer-region velocity profiles downstream of the separation. |
| NASA分類 | AERODYNAMICS |
| レポートNO | 84A27144 |
| 権利 | Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/398971 |
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