Span loaded flying wing control

Details Span loaded flying wing control Span loaded flying wing control

1980-12-01

1986-01-28

Blix, Trygve M.

Aeronautics and astronautics

Aircraft control

Rudders and empennage

244113, 244 87, 244215, 244 36, B64C 920, B64C 932, B64C 900

Patent

active

045666571

ABSTRACT:
A flying wing aircraft control for angle of attack and direction thereof, comprising retractile controlling surfaces rearward of the center of lift and along the trailing edges and extensible over the top and bottom cambers of the wing in spaced relation to the trailing portions thereof and with variable angular dispositions with respect to air flow over the cambers so as to establish the desired moment arm with respect to the lift center of the flying wing to control the same into and out of a nose-up attitude with respect to the line of flight and with respect to direction, as required.

REFERENCES:
patent: 2406506 (1946-08-01), Northrop
patent: 2431449 (1947-11-01), Ashkenas et al.
patent: 2650780 (1953-09-01), Northrup et al.
patent: 4040580 (1977-08-01), Schwaerzler

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