Add to ORKGA problem of modification of the classical airfoils that ensure the absence of separation in a subsonic ideal-gas flow in a specified range of angles of attack is solved by a numerical-analytical method based on the quasi-solution of inverse boundary-value problems of aerohydrodynamics and Kármán-Jiang formulas. Loitsyanskii's criterion of the non-separated flow is used to determine the boundary-layer separation point. © MAIK/Nauka 2008
Plane and two-dimensional inverse boundary-value problems of aerohydrodynamics (IBPA) have been inve...
The lift/drag ratio of an airfoil placed in an incompressible attached flow is maximized taking into...
The problem is solved of designing a symmetric airfoil with upstream blowing opposite to subsonic ir...
A problem of modification of the classical airfoils that ensure the absence of separation in a subso...
A numerical-analytical solution of an inverse boundary-value problem of aerohydrodynamics is obtaine...
A simple and reliable method of aerodynamic design of airfoils is proposed for a given range of the ...
Wing sections in a viscous subsonic flow with big Reynolds numbers are considered in the paper aimin...
A number of formulations and methods were proposed to solve variational inverse boundary-value probl...
Using the method of quasisolutions for inverse boundary-value problems of aerohydrodynamics, a probl...
We state and solve an optimization problem of finding a shape of airfoils with a separation-free flo...
Title: Solution of inverse problem for a flow around an airfoil Author: Mgr. Jan Šimák Department: D...
By the assumption that the pressure-volume relation is linear, a method is given for computing the a...
An exact solution of the problem of designing an airfoil with a prescribed velocity distribution on ...
An iteration method for airfoil shape completing using the pressure coefficient distribution specifi...
In the present work the method of the inverse boundary-value problems is used to obtain upper estima...
Plane and two-dimensional inverse boundary-value problems of aerohydrodynamics (IBPA) have been inve...
The lift/drag ratio of an airfoil placed in an incompressible attached flow is maximized taking into...
The problem is solved of designing a symmetric airfoil with upstream blowing opposite to subsonic ir...
A problem of modification of the classical airfoils that ensure the absence of separation in a subso...
A numerical-analytical solution of an inverse boundary-value problem of aerohydrodynamics is obtaine...
A simple and reliable method of aerodynamic design of airfoils is proposed for a given range of the ...
Wing sections in a viscous subsonic flow with big Reynolds numbers are considered in the paper aimin...
A number of formulations and methods were proposed to solve variational inverse boundary-value probl...
Using the method of quasisolutions for inverse boundary-value problems of aerohydrodynamics, a probl...
We state and solve an optimization problem of finding a shape of airfoils with a separation-free flo...
Title: Solution of inverse problem for a flow around an airfoil Author: Mgr. Jan Šimák Department: D...
By the assumption that the pressure-volume relation is linear, a method is given for computing the a...
An exact solution of the problem of designing an airfoil with a prescribed velocity distribution on ...
An iteration method for airfoil shape completing using the pressure coefficient distribution specifi...
In the present work the method of the inverse boundary-value problems is used to obtain upper estima...
Plane and two-dimensional inverse boundary-value problems of aerohydrodynamics (IBPA) have been inve...
The lift/drag ratio of an airfoil placed in an incompressible attached flow is maximized taking into...
The problem is solved of designing a symmetric airfoil with upstream blowing opposite to subsonic ir...