Yaw and pitch control of air vehicles at high angles of attack

Details Yaw and pitch control of air vehicles at high angles of attack Yaw and pitch control of air vehicles at high angles of attack

1987-01-05

1988-11-22

Barefoot, Galen

Aeronautics and astronautics

Aircraft control

244213, 244 45A, 244 91, B64C 1900

Patent

active

047860090

ABSTRACT:
Method and apparatus for controlling the yaw and pitch of air vehicles at high angles of attack by controlling the vortex pattern around the forebodies of the air vehicles by means of deflecting strakes 11 and 16.

REFERENCES:
patent: 2338935 (1944-01-01), Hafner
patent: 2448075 (1948-08-01), Bortner
patent: 2743888 (1956-05-01), Lippisch
patent: 4161300 (1979-07-01), Schwaerzler
patent: 4542866 (1985-09-01), Caldwell et al.
Sven, "A Device for Yawing Moment Control of Aircraft", European Patent Application, EP 0209171, Jan. 1987.

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