| タイトル | Wind tunnel results of the high-speed NLF(1)-0213 airfoil |
| 本文（外部サイト） | http://hdl.handle.net/2060/19900003226 |
| 著者（英） | Sewall, William G.; Jordan, Frank L., Jr.; Hahne, David E.; Mcghee, Robert J. |
| 著者所属（英） | NASA Langley Research Center |
| 発行日 | 1987-12-01 |
| 言語 | eng |
| 内容記述 | Wind tunnel tests were conducted to evaluate a natural laminar flow airfoil designed for the high speed jet aircraft in general aviation. The airfoil, designated as the High Speed Natural Laminar Flow (HSNLF)(1)-0213, was tested in two dimensional wind tunnels to investigate the performance of the basic airfoil shape. A three dimensional wing designed with this airfoil and a high lift flap system is also being evaluated with a full size, half span model. |
| NASA分類 | AERODYNAMICS |
| レポートNO | 90N12542 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/139873 |
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