| タイトル | Experimental results for the Eppler 387 airfoil at low Reynolds numbers in the Langley low-turbulence pressure tunnel |
| 本文（外部サイト） | http://hdl.handle.net/2060/19890001471 |
| 著者（英） | Mcghee, Robert J.; Millard, Betty F.; Walker, Betty S. |
| 著者所属（英） | NASA Langley Research Center |
| 発行日 | 1988-10-01 |
| 言語 | eng |
| 内容記述 | Experimental results were obtained for an Eppler 387 airfoil in the Langley Low Turbulence Pressure Tunnel. The tests were conducted over a Mach number range from 0.03 to 0.13 and a chord Reynolds number range for 60,000 to 460,000. Lift and pitching moment data were obtained from airfoil surface pressure measurements and drag data for wake surveys. Oil flow visualization was used to determine laminar separation and turbulent reattachment locations. Comparisons of these results with data on the Eppler 387 airfoil from two other facilities as well as the Eppler airfoil code are included. |
| NASA分類 | AERODYNAMICS |
| レポートNO | 89N10842
NAS 1.15:4062
L-16430
NASA-TM-4062 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/145018 |
