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Aircraft with Forward Sweeping T-TailAn aircraft includes a propulsor supported within an aft portion of the fuselage. A thrust reverser is supported proximate the propulsor for redirecting thrust forward to slow the aircraft upon landing. A tail extending from the aft portion of the fuselage is angled forward away from the aft portion and out of the discharge of airflow from the thrust reverser.
Document ID
20170004917
Acquisition Source
Headquarters
Document Type
Other - Patent
Authors
Suciu, Gabriel L.
Chandler, Jesse M.
Date Acquired
June 2, 2017
Publication Date
May 2, 2017
Subject Category
Aerodynamics
Funding Number(s)
CONTRACT_GRANT: NNX11AB35A
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Patent
US-Patent-9,637,218
Patent Application
US-Patent-Appl-SN-14/440,753

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