FIELD: aeronautical engineering flow break-away control device on straight wings. SUBSTANCE: flow is acted on by several extensible members mounted at some distance from one another inside flow-separation area along entire wing span in parallel with leading edge of wing in line of spreading of three-dimensional return current. Action of effected taking into account results of measurements of flow aerodynamic surface by means of sensors. EFFECT: increased lift force; enhanced efficiency of control. 3 dwg
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