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Determining the shape of an axisymmetric body in a viscous incompressible flow on the basis of the pressure distribution on the body surface, which involves the solutions of the inverse problem in the plane case and of the direct problem
Maximization of the lift coefficient of airfoils equipped with active flow control devices of inverse boundary-value problems of aerohydrodynamics. The initial problem with limitations is reduced
Approximate method of designing a two-element airfoil on reducing an inverse boundary-value problem in a doubly connected domain to a problem in a singly connected
Design of airfoils providing the absence of separation in a compressible flow in a specified range of angles of attack based on the quasi-solution of inverse boundary-value problems of aerohydrodynamics and Kármán
Determining the shape of an axisymmetric body in a viscous incompressible flow on the basis of the pressure distribution on the body surface, which involves the solutions of the inverse problem in the plane case and of the direct problem
Construction of an airfoil with an irregularity in the flowUsing the method of quasisolutions for inverse boundary-value problems of aerohydrodynamics, a
Exact solutions of basic variational inverse boundary value problem of aerohydrodynamicsThe problems of determining the maximum lift attainable on wing profile and the corresponding
Approximate method of designing a two-element airfoil on reducing an inverse boundary-value problem in a doubly connected domain to a problem in a singly connected
A boundary value problem of aerohydrodynamics in designing an axisymmetric body with jet blowout. The foundation of the method is the iteration process based on the solutions of an inverse problem in the plane
Design of airfoils providing the absence of separation in a compressible flow in a specified range of angles of attack based on the quasi-solution of inverse boundary-value problems of aerohydrodynamics and Kármán
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