| タイトル | High-flaps for natural laminar flow airfoils |
| 本文（外部サイト） | http://hdl.handle.net/2060/19880014355 |
| 著者（英） | Morgan, Harry L. |
| 著者所属（英） | NASA Langley Research Center |
| 発行日 | 1986-05-01 |
| 言語 | eng |
| 内容記述 | A review of the NACA and NASA low-drag airfoil research is presented with particular emphasis given to the development of mechanical high-lift flap systems and their application to general aviation aircraft. These flap systems include split, plain, single-slotted, and double-slotted trailing-edge flaps plus slat and Krueger leading-edge devices. The recently developed continuous variable-camber high-lift mechanism is also described. The state-of-the-art of theoretical methods for the design and analysis of multi-component airfoils in two-dimensional subsonic flow is discussed, and a detailed description of the Langley MCARF (Multi-Component Airfoil Analysis Program) computer code is presented. The results of a recent effort to design a single- and double-slotted flap system for the NASA high speed natural laminar flow (HSNLF) (1)-0213 airfoil using the MCARF code are presented to demonstrate the capabilities and limitations of the code. |
| NASA分類 | AERODYNAMICS |
| レポートNO | 88N23739 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/146227 |
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