Investigation of aerodynamic performance on low-aspect-ratio wings at low Reynolds numbers
The aerodynamic properties of the wing (drag, lift-to-drag ratio and induced drag) were investigated experimentally. Two forms of nonlinear equations of lift curves. Flow visualization in observing the influences of tip vortices shed from the wing tips.
| Рубрика | Физика и энергетика |
| Предмет | Gas dynamics |
| Вид | статья |
| Язык | английский |
| Прислал(а) | Fei-Bin Hsiao, Chi-Yu Lin, Yi-Chung and Di-Bao Wang, Chin-Yi Wei |
| Дата добавления | 18.01.2014 |
| Размер файла | 417,0 K |
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