Leaned and swept fan outlet guide vanes

A gas turbine engine assembly comprising:

• an annular fan duct circumscribed about a centerline,
• an annular core engine inlet disposed axially aft of said fan duct,
• an annular fan bypass inlet disposed axially aft of said fan duct and radially outward of said core engine inlet,
• an annular splitter disposed radially between said fan bypass inlet and said core engine inlet,
• a plurality of axially swept fan exit guide vanes having axially swept vane trailing edges and circumferentially disposed around said centerline and within said fan duct with only an axially extending gap between said fan exit guide vanes and strut leading edges of said struts,
• a plurality of struts having axially swept strut leading edges, circumferentially disposed around said centerline, and disposed radially across said fan bypass inlet and said core engine inlet,
• said fan exit guide vanes comprising axially swept vane airfoils having pressure and suction sides, radially spanning outward across said fan duct from vane airfoil roots to vane airfoil tips, and extending axially aft from vane leading edges to said vane trailing edges, and
• said vane airfoils having a circumferential lean such that said pressure sides face radially inward.