An asymmetric aircraft configuration having a first and a second wing, the first wing having a span larger than the second wing. A first engine is mounted on the first wing, and a second engine mounted on the rear end of the aircraft with its centerline aligned with the aircraft longitudinal axis. The rear end of the aircraft has a T tail, and the second engine is configured to ingest and consume air forming a boundary layer during the flight. A main landing gear assembly includes a first landing gear attached to the first wing, and a second landing gear attached to an area of the fuselage close to the second wing.
ASYMMETRIC AIRCRAFT CONFIGURATION
2021-09-16
Patent
Electronic Resource
English
Flight Testing of Eurofighter Aircraft in the Asymmetric GBU-10 Configuration
British Library Conference Proceedings | 2005
|Wiley | 2000
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