| タイトル | Experimental and theoretical low speed aerodynamic characteristics of the NACA 65 sub 1-213, alpha equals 0.50, airfoil |
| 本文（外部サイト） | http://hdl.handle.net/2060/19750007534 |
| 著者（英） | Mcghee, R. J.; Beasley, W. D. |
| 著者所属（英） | NASA Langley Research Center |
| 発行日 | 1975-02-01 |
| 言語 | eng |
| 内容記述 | Low-speed wind-tunnel tests have been conducted to determine the two-dimensional aerodynamic characteristics of the NACA 65 sub 1-213, a = 0.05, airfoil. The results were compared with data from another low-speed wind tunnel and also with theoretical predictions obtained by using a viscous subsonic method. The tests were conducted over a Mach number range from 0.10 to 0.36. Reynolds numbers based on the airfoil chord varied from about 3 million to 23 million. |
| NASA分類 | AERONAUTICS (GENERAL) |
| レポートNO | 75N15606
NASA-TM-X-3160
L-9773 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/191424 |
