POSSIBILITY OF LEADTHROUGH OF RESEARCHES OF CONTROL TWIST AND CURVATURE OF TYPE THICK ON BASIS OF WING OF MODERN HANG-GLIDER

A.N. Tykhovskyi

In the constructions of modern aircrafts it is accepted to influence on aerodynamic properties of their wings by various facilities of mechanization. Thus the in-use are not used yet on sunset the aviation of mean of curvature of type and possibilities are not investigational on a direct management a thickness and curvature of type. A hang-glider, passing the stages of development as aircraft, saved some limited flexibility of the wing. It enables, applying the special facilities of change of twist covered, his thicknesses and curvatures of middle line of type, to use hang-gliders covered for implementation of complex of researches on influence of direct control profiling on his aerodynamic properties

Key words: wind tunnel, hang-glider, twist wing, control profiling.