| タイトル | Natural laminar flow flight experiments on a swept-wing business jet |
| 著者（英） | Wentz, W. H., Jr.; Nyenhuis, R.; Ahmed, A. |
| 著者所属（英） | Cessna Aircraft Co.; Wichita State Univ. |
| 発行日 | 1984-08-01 |
| 言語 | eng |
| 内容記述 | Flight test experiments have been conducted to measure the extent and nature of laminar flow on a smoothed test region of a swept-wing business jet. Surface hot film anemometers and sublimating chemicals were used for transition detection. Surface pressure distributions were measured using pressure belts. Instrumentation techniques and problems are presented. Correlation was obtained between the hot film and sublimating chemicals for transition detection. Taylor-Goertler vortices were observed for some flight conditions. Boundary layer stability analysis is being conducted using measured pressure distributions to determine the correlation possible for transition prediction on swept wings. |
| NASA分類 | AERODYNAMICS |
| レポートNO | 84A41344
AIAA PAPER 84-2189 |
| 権利 | Copyright |
