| タイトル | Low-speed aerodynamic characteristics of a 9.3-percent-thick supercritical airfoil section |
| 本文（外部サイト） | http://hdl.handle.net/2060/19830002798 |
| 著者（英） | Mcghee, R. J.; Noonan, K. W. |
| 著者所属（英） | NASA Langley Research Center |
| 発行日 | 1982-08-01 |
| 言語 | eng |
| 内容記述 | An investigation was conducted in the Langley low turbulence pressure tunnel to determine the low-speed, two dimensional characteristics of a 9.3 percent-thick supercritical airfoil. The airfoil was tested at Reynolds numbers (based on chord) from 2.9 million to 16.8 million, at Mach numbers from 0.10 to 0.36, and at geometric angles of attack from -8 degrees to 14 degrees. |
| NASA分類 | AERODYNAMICS |
| レポートNO | 83N11068
NASA-TM-X-72763
NAS 1.15:X-72763 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/164483 |
