FIELD: design of supersonic aircraft. SUBSTANCE: all-moving wing 1 is formed beyond boundaries of fuselage by two wing panels 2 and 3 which are swivel relative to longitudinal axis of wing. Deflection of panels is effected in synchronism and separately through angle of attack α changing from -90 deg to aw corresponding to maximum lift γmax. EFFECT: enhanced efficiency. 3 dwg
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|
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| AIRCRAFT | 2014 |
|
RU2577824C1 |
