AbstractIn the paper there are solved direct and inverse boundary problems and analytical solutions are obtained for optimization problems in the case of some nonlinear integral operators. It is modeled the plane potential flow of an inviscid, incompressible and nonlimited fluid jet, witch encounters a symmetrical, curvilinear obstacle—the deflector of maximal drag. There are derived integral singular equations, for direct and inverse problems and the movement in the auxiliary canonical half-plane is obtained. Next, the optimization problem is solved in an analytical manner. The design of the optimal airfoil is performed and finally, numerical computations concerning the drag coefficient and other geometrical and aerodynamical parameters ar...
This paper attempts to determine the optimum profile of a two-dimensional plate that produces the ma...
An inverse boundary value problem of aerodynamics is formulated and solved for an ekranoplan airfoil...
The potential flow through an infinite cascade of aerofoils is considered as both a direct and inver...
In this paper the problem of finding the impermeable parachute of optimum shape in a subsonic gas fl...
A simple, two dimensional, incompressible and inviscid model for the problem posed by a two dimensio...
AbstractA model of Helmholtz type for a plane inviscid incompressible and potential fluid flow past ...
The problem of potential flow around two-dimensional airfoils is solved by using a new singular inte...
We state and solve an optimization problem of finding a shape of airfoils with a separation-free flo...
The lift/drag ratio of an airfoil placed in an incompressible attached flow is maximized taking into...
A number of formulations and methods were proposed to solve variational inverse boundary-value probl...
AbstractIn the classical two-dimensional model the description of Helmholtz's (Kirchhoff) flow is a ...
A simple and reliable method of aerodynamic design of airfoils is proposed for a given range of the ...
The minimization of inviscid fluid drag is studied for aerodynamic shapes satisfying the conditions ...
PART I In a recent paper Wu, T.Y. & Whitney, A.K., the authors studied optimum shape problems in hyd...
In this paper we develop a method for constructing a quasisolution to the inverse boundary value pro...
This paper attempts to determine the optimum profile of a two-dimensional plate that produces the ma...
An inverse boundary value problem of aerodynamics is formulated and solved for an ekranoplan airfoil...
The potential flow through an infinite cascade of aerofoils is considered as both a direct and inver...
In this paper the problem of finding the impermeable parachute of optimum shape in a subsonic gas fl...
A simple, two dimensional, incompressible and inviscid model for the problem posed by a two dimensio...
AbstractA model of Helmholtz type for a plane inviscid incompressible and potential fluid flow past ...
The problem of potential flow around two-dimensional airfoils is solved by using a new singular inte...
We state and solve an optimization problem of finding a shape of airfoils with a separation-free flo...
The lift/drag ratio of an airfoil placed in an incompressible attached flow is maximized taking into...
A number of formulations and methods were proposed to solve variational inverse boundary-value probl...
AbstractIn the classical two-dimensional model the description of Helmholtz's (Kirchhoff) flow is a ...
A simple and reliable method of aerodynamic design of airfoils is proposed for a given range of the ...
The minimization of inviscid fluid drag is studied for aerodynamic shapes satisfying the conditions ...
PART I In a recent paper Wu, T.Y. & Whitney, A.K., the authors studied optimum shape problems in hyd...
In this paper we develop a method for constructing a quasisolution to the inverse boundary value pro...
This paper attempts to determine the optimum profile of a two-dimensional plate that produces the ma...
An inverse boundary value problem of aerodynamics is formulated and solved for an ekranoplan airfoil...
The potential flow through an infinite cascade of aerofoils is considered as both a direct and inver...