| タイトル | Low speed aerodynamic characteristics of NACA 6716 and NACA 4416 airfoils with 35 percent-chord single-slotted flaps |
| 本文（外部サイト） | http://hdl.handle.net/2060/19740013521 |
| 著者（英） | Noonan, K. W.; Bingham, G. J. |
| 著者所属（英） | NASA Langley Research Center|Army Air Mobility Research and Development Lab. |
| 発行日 | 1974-05-01 |
| 言語 | eng |
| 内容記述 | An investigation was conducted in a low-turbulence pressure tunnel to determine the two-dimensional lift and pitching-moment characteristics of an NACA 6716 and an NACA 4416 airfoil with 35-percent-chord single-slotted flaps. Both models were tested with flaps deflected from 0 deg to 45 deg, at angles of attack from minus 6 deg to several degrees past stall, at Reynolds numbers from 3.0 million to 13.8 million, and primarily at a Mach number of 0.23. Tests were also made to determine the effect of several slot entry shapes on performance. |
| NASA分類 | AERODYNAMICS |
| レポートNO | 74N21634
NASA-TM-X-2623
L-8410 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/195023 |
