| タイトル | Experimental study of the separating confluent boundary-layer. Volume 2: Experimental data |
| 本文（外部サイト） | http://hdl.handle.net/2060/19840012413 |
| 著者（英） | Jones, G. S.; Braden, J. A.; Lilley, D. E.; Whipkey, R. R. |
| 著者所属（英） | Lockheed-Georgia Co. |
| 発行日 | 1983-03-01 |
| 言語 | eng |
| 内容記述 | An experimental low speed study of the separating confluent boundary layer on a NASA GAW-1 high lift airfoil is described. The airfoil was tested in a variety of high lift configurations comprised of leading edge slat and trailing edge flap combinations. The primary test instrumentation was a two dimensional laser velocimeter (LV) system operating in a backscatter mode. Surface pressures and corresponding LV derived boundary layer profiles are given in terms of velocity components, turbulence intensities and Reynolds shear stresses as characterizing confluent boundary layer behavior up to and beyond stall. LV derived profiles and associated boundary layer parameters and those obtained from more conventional instrumentation such as pitot static transverse, Preston tube measurements and hot-wire surveys are compared. |
| NASA分類 | AERODYNAMICS |
| レポートNO | 84N20481
LG82ER0184
NASA-CR-166018
NAS 1.26:166018 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/159982 |
