An aircraft (10) comprising a fuselage (12), the fuselage (10) comprising at least first and second inwardly tapering portions (20, 22) extending in a generally rearward direction from an aft end of the fuselage (12), each inwardly tapering portion (20, 22) comprising a boundary layer ingesting propulsor (36) mounted thereon.
An aircraft with fuselage aft end tapering portions and boundary layer ingesting propulsors
2018-01-10
Patent
Electronic Resource
English