| 摘要 |
FIELD: aeronautical engineering and design of high-speed supersonic aircraft. SUBSTANCE: all-moving wing 1 is formed beyond fuselage limits with two wing panels 2 and 3 turnable relative to longitudinal axis of wing; displacement of these panels both simultaneously and separately is effected through angle of attack α, which changes from -90 deg to d, corresponding to maximum lifting force Y. EFFECT: reduction of takeoff and landing distances of aircraft; simplification of construction of landing gear legs; simplification of construction of wing; reduction of area of horizontal tail; enhanced maneuverability of aircraft. 3 dwg |
