| タイトル | The analysis and design of transonic two-element airfoil systems |
| 本文（外部サイト） | http://hdl.handle.net/2060/19790011871 |
| 著者（英） | Volpe, G.; Grossman, B. |
| 著者所属（英） | Grumman Aerospace Corp. |
| 発行日 | 1979-01-01 |
| 言語 | eng |
| 内容記述 | The multiphase effort in the development of tools for the analysis and design of two-element airfoil systems, that is, airfoils with a slat or a flap at transonic speeds is described. The first phase involved the development of a method to compute the inviscid flow over such configurations. In the second phase the inviscid code was coupled to a boundary layer calculation program in order to compute the loss in performance due to viscous effects. An inverse code that constructs the airfoil system corresponding to a desired pressure distribution is described. |
| NASA分類 | AERODYNAMICS |
| レポートNO | 79N20042 |
| 権利 | No Copyright |
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