title: Numerical and analytical modeling of the propulsive wing and fuselage of an air taxi
abstract: The problem of creating propulsive airfoils is considered. Such airfoils have a slit through which the boundary layer is sucked out. Located just behind this gap, a specially profiled section of the airfoil creates a propulsive thrust. The thrust is created due to an abrupt change in the pressure profile on the slit through which the boundary layer is sucked. In the last 15–20 years, the concept of a so-called propulsive wing with reduced or zero aerodynamic drag due to the suction of the bounda
journal: Scientific and technical journal of information technologies mechanics and optics