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Крыло самолета изменяемой в полете геометрии, состоящее из центроплана и поворотных консолей, которые разделены по размаху на ряд отдельных частей, шарнирно сопряженных с центропланом, отличающееся тем, что, с целью уменьшения нагрузок на шарниры крепления поворотных консолей и увеличения жесткости крыла, отдельные части поворотных консолей последнего шарнирно сочленены между собой по законцовке крыла.
SU1453709/23A1970-07-091970-07-09Крыло самолета изменяемой в полете геометрии
SU343538A1
(ru)
Application of low drag-due-to-lift concept of linearized theory to the studies of twist and camber of isolated wing and wing-body configurations of supersonic aircraft
Research works on high speed rotorcraft and the concept of retractable rotors(Flight characteristics of operational and experimental rotary wing aircraft analyzed to improve range and cruising speed)
The effect of wing twist distortion on glider static longitudinal stability with stick fixed(Wing twist distortion effect on glider static longitudinal stability with stick fixed)
Harmonic oscillatory motion of the conical wing-fuselage system under supersonic conditions(Unsteady supersonic flow about conical wing fuselage system with LF harmonic oscillatory motion)
Downwash tests of the dual tandem ducted propeller VTOL research aircraft configurations to evaluate engine inlets, protection devices and study aerodynamic interference(Downwash tests of dual tandem ducted propeller VTOL research aircraft configurations to evaluate engine inlets, protection devices and study aerodynamic interference)
Helicopter noise: Blade slap. Part 2: Experimental results(Flight tests to determine characteristics of blade slap in rotary wings and effect on helicopter performance)