Aircraft

Claim 1

In a supercritical wing having a large leading edge radius of curvature directly followed chordwise on the upper surface by a curvature transition region and then a directly following low positive curvature region extending for 30% to 90% of the chord, and on the lower surface by a forward region of curvature generally larger than that of the upper surface low curvature region, a transition region characterised by an inflexion and occurring between 50% and 70% chord, and then a rearward region of concave curvature, the improvement comprising a knee in said upper surface curvature transition region, located at between 3% and 13% chord and extending continuously over a substantial portion of the span of the wing, said knee being characterised by a curvature which is positively greater than that immediately forward and that immediately rearward thereof, and said knee being operative to contain the peak velocity and suction at low speeds and thereby to delay the onset of stall, to minimise local supersonic expansion at intermediate speeds, and to create a region of high expansion stabilised over the knee at supercritical speeds.