| タイトル | KC-135 winglet program overview |
| 著者（英） | Selegan, D.; Barber, M. R. |
| 著者所属（英） | NASA Dryden Flight Research Center |
| 発行日 | 1982-01-01 |
| 言語 | eng |
| 内容記述 | A joint NASA/USAF program was conducted to accomplish the following objectives: (1) evaluate the benefits that could be achieved from the application of winglets to KC-135 aircraft; and (2) determine the ability of wind tunnel tests and analytical analysis to predict winglet characteristics. The program included wind-tunnel development of a test winglet configuration; analytical predictions of the changes to the aircraft resulting from the application of the test winglet; and finally, flight tests of the developed configuration. Pressure distribution, loads, stability and control, buffet, fuel mileage, and flutter data were obtained to fulfill the objectives of the program. |
| NASA分類 | AERODYNAMICS |
| レポートNO | 84N27687 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/529815 |
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