AIRCRAFT LIFTING SURFACE WITH VARIABLE SWEEP DISTRIBUTION ALONG THE SPAN

摘要

An aircraft lifting surface attached to the rear or frontal end of the aircraft fuselage with a variable sweep angleαin an inboard part and with a constant sweep angleα1 in an outboard part. The aircraft lifting surface can be for example a horizontal tail plane or a vertical tail plane attached to the rear end fuselage or a canard attached to the frontal end fuselage.