AbstractIn this paper we develop a fast Petrov–Galerkin method for solving the generalized airfoil equation using the Chebyshev polynomials. The conventional method for solving this equation leads to a linear system with a dense coefficient matrix. When the order of the linear system is large, the computational complexity for solving the corresponding linear system is huge. For this we propose the matrix truncation strategy, which compresses the dense coefficient matrix into a sparse matrix. We prove that the truncated method preserves the optimal order of the approximate solution for the conventional method. Moreover, we solve the truncated equation using the multilevel augmentation method. The computational complexity for solving this tru...
AbstractIn this paper we consider new error estimates under the weighted Chebyshev norm for Galerkin...
In this paper, we present a fast, ecient and accurate algorithm for rapid design of sub-critical inv...
Multigrid technique has been tried to solve the Full Potential Equation on an airfoil in Cartesian g...
AbstractIn this paper we develop a fast Petrov–Galerkin method for solving the generalized airfoil e...
AbstractThe authors consider the generalized airfoil equation in some weighted Hölder–Zygmund spaces...
The authors consider the generalized airfoil equation in some weighted Hölder–Zygmund spaces with un...
An efficient multi-block Newton–Krylov algo-rithm using the compressible Navier–Stokes equations is ...
An efficient multi-block Newton--Krylov algorithm using the compressible Navier--Stokes equations is...
AbstractIn this paper we establish the L2 convergence of a polynomial collocation method for the sol...
Abstract—In this paper, we introduce a generalized Chebyshev collocation method (GCCM) based on the ...
An iteration method for airfoil shape completing using the pressure coefficient distribution specifi...
SIGLEAvailable from TIB Hannover: RR 5549(242)+a / FIZ - Fachinformationszzentrum Karlsruhe / TIB - ...
This thesis is concerned with aerodynamic optimization of airfoils and wings. It focuses at using ve...
Multigrid technique is a method which accelerates the convergence and hence reduces the CPU time for...
The Multigrid technique is 'employed to,get the fast convergence of solutions for the algorithms par...
AbstractIn this paper we consider new error estimates under the weighted Chebyshev norm for Galerkin...
In this paper, we present a fast, ecient and accurate algorithm for rapid design of sub-critical inv...
Multigrid technique has been tried to solve the Full Potential Equation on an airfoil in Cartesian g...
AbstractIn this paper we develop a fast Petrov–Galerkin method for solving the generalized airfoil e...
AbstractThe authors consider the generalized airfoil equation in some weighted Hölder–Zygmund spaces...
The authors consider the generalized airfoil equation in some weighted Hölder–Zygmund spaces with un...
An efficient multi-block Newton–Krylov algo-rithm using the compressible Navier–Stokes equations is ...
An efficient multi-block Newton--Krylov algorithm using the compressible Navier--Stokes equations is...
AbstractIn this paper we establish the L2 convergence of a polynomial collocation method for the sol...
Abstract—In this paper, we introduce a generalized Chebyshev collocation method (GCCM) based on the ...
An iteration method for airfoil shape completing using the pressure coefficient distribution specifi...
SIGLEAvailable from TIB Hannover: RR 5549(242)+a / FIZ - Fachinformationszzentrum Karlsruhe / TIB - ...
This thesis is concerned with aerodynamic optimization of airfoils and wings. It focuses at using ve...
Multigrid technique is a method which accelerates the convergence and hence reduces the CPU time for...
The Multigrid technique is 'employed to,get the fast convergence of solutions for the algorithms par...
AbstractIn this paper we consider new error estimates under the weighted Chebyshev norm for Galerkin...
In this paper, we present a fast, ecient and accurate algorithm for rapid design of sub-critical inv...
Multigrid technique has been tried to solve the Full Potential Equation on an airfoil in Cartesian g...