| 摘要 |
<p>An aircraft wing assembly, comprising a front spar, a rear spar (9'), and upper and lower wing covers extending between the front and rear spars, wherein the upper and/or lower wing cover (3') overhangs the rear spar (9') and has a non-linear trailing edge profile forming an array of tabs (17a,17b) and cut-outs (18). Also, a method of assembling the aircraft wing.</p> |
