The authors consider the generalized airfoil equation in some weighted Hölder–Zygmund spaces with uniform norms. Using a projection method based on the de la Vallée Poussin interpolation, they reproduce the estimates of the L2 case by cutting off the typical extra logm factor which seemed inevitable to have dealing with the uniform norm, because of the unboundedness of the Lebesgue constants. The better convergence estimates do not produce a greater computational effort: the proposed numerical procedure leads to solve a simple tridiagonal linear system, the condition number of which tends to a finite limit as the dimension of the system tends to infinity, whatever natural matrix norm is considered. Several numerical tests are given
In the aeronautical applications, many problems involving boundaries of unspecified geometry are of ...
An iteration method for airfoil shape completing using the pressure coefficient distribution specifi...
The problem of the accuracy improving is considered for vortex method. The general Galerkin-type app...
AbstractThe authors consider the generalized airfoil equation in some weighted Hölder–Zygmund spaces...
AbstractIn this paper we develop a fast Petrov–Galerkin method for solving the generalized airfoil e...
AbstractIn this paper we establish the L2 convergence of a polynomial collocation method for the sol...
The airfoil equation is considered over two disjoint intervals. Assuming the distance between the in...
AbstractIn this paper we consider new error estimates under the weighted Chebyshev norm for Galerkin...
SIGLEAvailable from TIB Hannover: RR 5549(242)+a / FIZ - Fachinformationszzentrum Karlsruhe / TIB - ...
In this paper we discuss a novel accurate method for computing transonic flow over lifting and non-l...
AbstractIn this paper we consider for the classical airfoil equation a collocation method based on J...
In order to solve Prandtl-type equations we propose a collocation-quadrature method based on de la V...
An efficient multi-block Newton–Krylov algo-rithm using the compressible Navier–Stokes equations is ...
The Multigrid technique is 'employed to,get the fast convergence of solutions for the algorithms par...
"On the assumption of infinitely small disturbances the author develops a generalized integral equat...
In the aeronautical applications, many problems involving boundaries of unspecified geometry are of ...
An iteration method for airfoil shape completing using the pressure coefficient distribution specifi...
The problem of the accuracy improving is considered for vortex method. The general Galerkin-type app...
AbstractThe authors consider the generalized airfoil equation in some weighted Hölder–Zygmund spaces...
AbstractIn this paper we develop a fast Petrov–Galerkin method for solving the generalized airfoil e...
AbstractIn this paper we establish the L2 convergence of a polynomial collocation method for the sol...
The airfoil equation is considered over two disjoint intervals. Assuming the distance between the in...
AbstractIn this paper we consider new error estimates under the weighted Chebyshev norm for Galerkin...
SIGLEAvailable from TIB Hannover: RR 5549(242)+a / FIZ - Fachinformationszzentrum Karlsruhe / TIB - ...
In this paper we discuss a novel accurate method for computing transonic flow over lifting and non-l...
AbstractIn this paper we consider for the classical airfoil equation a collocation method based on J...
In order to solve Prandtl-type equations we propose a collocation-quadrature method based on de la V...
An efficient multi-block Newton–Krylov algo-rithm using the compressible Navier–Stokes equations is ...
The Multigrid technique is 'employed to,get the fast convergence of solutions for the algorithms par...
"On the assumption of infinitely small disturbances the author develops a generalized integral equat...
In the aeronautical applications, many problems involving boundaries of unspecified geometry are of ...
An iteration method for airfoil shape completing using the pressure coefficient distribution specifi...
The problem of the accuracy improving is considered for vortex method. The general Galerkin-type app...