Patent ID: 7883052

Claim:
A wing, comprising: an inboard section adapted to be attached on one side thereof to a fuselage and adapted to be attached on an opposing side thereof to an inboard side of an engine nacelle in an over-the-wing mounting position, said inboard section having a leading edge and a trailing edge; an outboard section adapted to be attached on one side thereof to an outboard side of said nacelle, said outboard section having a leading edge and a trailing edge; said outboard section leading edge having a sweep of at least 20 degrees; said inboard section leading edge having a sweep between −15 and +15 degrees; and said inboard section leading edge extending from said fuselage to an attachment position on said nacelle, wherein the attachment position on said fuselage and said attachment position on said nacelle are forward of an index position on the inboard side of said nacelle, said index position defined as an imaginary intersection between said sweep of said outboard section and said inboard side of said nacelle.