| タイトル | A critical evaluation of the predictions of the NASA-Lockheed multielement airfoil computer program |
| 本文（外部サイト） | http://hdl.handle.net/2060/19780012133 |
| 著者（英） | Manke, J. W.; Brune, G. W. |
| 著者所属（英） | Boeing Commercial Airplane Co. |
| 発行日 | 1978-03-01 |
| 言語 | eng |
| 内容記述 | Theoretical predictions of several versions of the multielement airfoil computer program are evaluated. The computed results are compared with experimental high lift data of general aviation airfoils with a single trailing edge flap, and of airfoils with a leading edge flap and double slotted trailing edge flaps. Theoretical and experimental data include lift, pitching moment, profile drag and surface pressure distributions, boundary layer integral parameters, skin friction coefficients, and velocity profiles. |
| NASA分類 | AERODYNAMICS |
| レポートNO | 78N20076
D6-45100
NASA-CR-145322 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/179488 |
