| 摘要 |
<p>The invention relates to the wing of a flying apparatus and a flying apparatus, the leading edge of which wing is at least partly at a sweep, on which leading edge part at a sweep are arranged means (2, 2') which, when activated, raise controls (3) generating vortices on the upper surface of the wing and which at the same time increase the degree of curvature of the mean chord (6) of the airfoil in the leading edge area of the wing.</p> |
