Aircraft

Aeronautics and astronautics – Aircraft sustentation – Sustaining airfoils

Patent

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Details

244113, B64C 358, B64C 932

Patent

active

049559583

ABSTRACT:
An aircraft with no separate elevators in the tail end of the fuselage and having wings arranged approximately in the middle portion of the fuselage, is improved by a single flap on the underside of the wings for extending down to a variable degree and being arranged at a point between 49 and 54% of the local chord depth as measured from the leading edge.

REFERENCES:
patent: 2205714 (1940-06-01), Doepp

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