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
Вид статья
Язык английский
Дата добавления 18.01.2014
Размер файла 417,0 K

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