| タイトル | On the design of airfoils in which the transition of the boundary layer is delayed |
| 本文（外部サイト） | http://hdl.handle.net/2060/19930093879 |
| 著者（英） | Tani, Itiro |
| 著者所属（英） | National Advisory Committee for Aeronautics |
| 発行日 | 1952-10-01 |
| 言語 | eng |
| 内容記述 | A method is presented for designing suitable thickness distributions and mean camber lines for airfoils permitting extensive chordwise laminar flow. Wind tunnel and flight tests confirming the existence of laminar flow; possible maintenance of laminar flow by area suction; and the effects of wind tunnel turbulence and surface roughness on the promotion of premature boundary layer transition are discussed. In addition, estimates of profile drag and scale effect on maximum lift of the derived airfoils are made. |
| レポートNO | 93R23204
NACA-TM-1351 |
| 権利 | No Copyright |
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