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
16.09.2021
Patent
Elektronische Ressource
Englisch
Flight Testing of Eurofighter Aircraft in the Asymmetric GBU-10 Configuration
British Library Conference Proceedings | 2005
|Wiley | 2000
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