| タイトル | Wind tunnel testing of low-drag airfoils |
| 本文（外部サイト） | http://hdl.handle.net/2060/19880014357 |
| 著者（英） | Harris, C. D.; Harvey, W. Donald; Mcghee, R. J. |
| 著者所属（英） | NASA Langley Research Center |
| 発行日 | 1986-05-01 |
| 言語 | eng |
| 内容記述 | Results are presented for the measured performance recently obtained on several airfoil concepts designed to achieve low drag by maintaining extensive regions of laminar flow without compromising high-lift performance. The wind tunnel results extend from subsonic to transonic speeds and include boundary-layer control through shaping and suction. The research was conducted in the NASA Langley 8-Ft Transonic Pressure Tunnel (TPT) and Low Turbulence Pressure Tunnel (LTPT) which have been developed for testing such low-drag airfoils. Emphasis is placed on identifying some of the major factors influencing the anticipated performance of low-drag airfoils. |
| NASA分類 | AERODYNAMICS |
| レポートNO | 88N23741 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/146225 |
