| タイトル | Effect of camber on the trimmed lift capability of a close-coupled canard-wing configuration |
| 本文（外部サイト） | http://hdl.handle.net/2060/19780020109 |
| 著者（英） | Gloss, B. B. |
| 著者所属（英） | NASA Langley Research Center |
| 発行日 | 1978-07-01 |
| 言語 | eng |
| 内容記述 | A close-coupled canard-wing configuration was tested in the Langely high-speed 7 by 10 foot tunnel at a Mach number of 0.30 to determine the effect of changing wing camber on the trimmed lift capability. Trimmed lift coefficients of near 2.0 were attained; however, the data indicated that the highest buffet-free trimmed lift coefficient attainable was approximately 1.30. The buffet used in this investigation were qualitative in nature and gave no indication of buffet intensity. Thus, the trimmed lift coefficient of near 2.0 might be attainable if the buffet intensity was not too high. The data showed that there was approximately a 10 percent variation in drag coefficient, for different model configurations, at a given trimmed lift coefficient. Large increases in wing lift had only small effects on canard lift. |
| NASA分類 | AERODYNAMICS |
| レポートNO | 78N28052
NASA-TM-78686
L-12102 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/178313 |
