| タイトル | Profile design for an advanced-technology airfoil for general aviation aircraft |
| 本文（外部サイト） | http://hdl.handle.net/2060/19780024111 |
| 著者（英） | Welte, D. |
| 著者所属（英） | NASA Headquarters |
| 発行日 | 1978-08-01 |
| 言語 | eng |
| 内容記述 | A profile from the NASA General Aviation Whitcomb series and NACA profiles are used as a starting point in designing an advanced airfoil for general aviation aircraft. Potential theory pressure distribution calculations, together with boundary layer calculations, permit a decrease in the null moment and an optimization of the lift characteristics of the wing. Trailing edge flap design is also improved. Wind tunnel tests are used to compare the conventional profiles, the NASA profile, and the improved design. |
| NASA分類 | AERODYNAMICS |
| レポートNO | 78N32054
NASA-TM-75323
PAPER-77-027 |
| 権利 | No Copyright |
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