| タイトル | Static and unsteady pressure measurements on a 50 degree clipped delta wing at M = 0.9 |
| 著者（英） | Hess, R. W.; Wynne, E. C.; Cazier, F. W. |
| 著者所属（英） | NASA Langley Research Center |
| 発行日 | 1982-01-01 |
| 言語 | eng |
| 内容記述 | Static and unsteady pressures were measured on a 50.45 degree clipped delta wing in the Langley Transonic Dynamics Tunnel with Freon as the test medium. Data taken at M = 0.9 is presented for static and oscillatory deflections of the trailing edge control surface and for the wing in pitch. Comparisons of the static measured data are made with results computed using the Bailey-Ballhaus small disturbance code. |
| NASA分類 | AERODYNAMICS |
| レポートNO | 82A30153
AIAA PAPER 82-0686 |
| 権利 | Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/411015 |
