FIELD: aircraft engineering.
SUBSTANCE: in compliance with the first version, aircraft comprises wing with ailerons and tail unit with rudders. Every outer wing and/or tail unit has one or more ailerons and/or rudders that can independently deviate. In compliance with the second version, aircraft landing gear front leg accommodates aerodynamic vertical rudder..
EFFECT: provision of asymmetric aerodynamic drag to produce lateral sliding.
9 cl, 5 dwg
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Authors
Dates
2010-09-27—Published
2008-06-23—Filed