M. : PHYSMATLIT, 2011. — 404 s. The monograph summarizes and systematizes the results of studies of inkjet systems for increasing the lift power of wings performed at TsAGI, as well as published in domestic and foreign publications over the past 30-40 years. Control systems of the boundary layer and circulation by tangential blowing of jets on the wing are considered , flaps and rounded cylindrical tail part of the wing, inkjet and ejector flaps, Blowing system over the wing , from its ends , Ways to control artificially created flow separation on the wing. The results of experimental studies of inkjet systems on large-scale models and full-scale aircraft for various purposes, performed in a large wind tunnel T-101 TsAGI, as well as on profiles and wings of various shapes in other pre- and subsonic wind tunnels . are presented. Methods for calculating the aerodynamic characteristics of Wings with inkjet mechanization are presented and a comparison of the results of calculations with experimental data is given. The monograph is intended by developers of aviation equipment and scientific and technical workers specializing in the field of aerodynamics of aircraft. It can serve as a reference and educational guide for teachers, graduate students and students of aviation universities, as well as for all interested in aviation.