The accuracy of numerical solutions for the incompressible turbulent boundary layer past a flat plate is addressed by means of a prior and a posteriori analysis. The former is carried out by computing the exact solutions of the Reynolds averaged Navier-Stokes equations with the Baldwin-Lomax and Spalart-Allmaras models; these solutions are used for the truncation error estimate in the modified equations. The latter is performed by applying a generalized Richardson extrapolation to the numerical solutions computed by two different finite volume techniques, namely a centered scheme with artificial dissipation and a ENO-type scheme. The results of the a priori theoretical analysis were confirmed by a posteriori analysis of numerical sol...
There is a large variety of numerical methods that are used to solve the many flow problems to which...
An efficient procedure for solving the fully linearized form of the boundary-layer equations is desc...
In order to handle turbulent flow problems, one equation turbulence models are implemented in to a p...
The influence of turbulence model and numerical technique on RANS computations is discussed in the c...
AbstrAct: The present work is primarily concerned with studying the effects of artificial dissipatio...
The calculation of the turbulent boundary layer is performed when a steady flow of a viscous fluid ...
. In this article we consider grid approximations of a boundary value problem for boundary layer equ...
ABSTRACT: The present work is primarily concerned with studying the effects of artificial dissipatio...
A detailed grid convergence study has been conducted to establish accurate reference solutions corre...
Computation of Airfoil boundary layer is an analysis of flow around an airfoil using a CFD commercia...
Runge-Kutta/Implicit methods for the solution of the Navier-Stokes equations provide superior conver...
The Backward Differentiation Formulae (BDF) of orders one to six are implemented in an in-house thre...
Abstract. Textbook multigrid efficiencies for high Reynolds number simulations based on the incom-pr...
International audienceThe aim of this work is to contribute to the understanding of sensitivity of b...
Reynolds Averaged Navier Stokes (RANS) equations are solved using third order upwind biased Roe's sc...
There is a large variety of numerical methods that are used to solve the many flow problems to which...
An efficient procedure for solving the fully linearized form of the boundary-layer equations is desc...
In order to handle turbulent flow problems, one equation turbulence models are implemented in to a p...
The influence of turbulence model and numerical technique on RANS computations is discussed in the c...
AbstrAct: The present work is primarily concerned with studying the effects of artificial dissipatio...
The calculation of the turbulent boundary layer is performed when a steady flow of a viscous fluid ...
. In this article we consider grid approximations of a boundary value problem for boundary layer equ...
ABSTRACT: The present work is primarily concerned with studying the effects of artificial dissipatio...
A detailed grid convergence study has been conducted to establish accurate reference solutions corre...
Computation of Airfoil boundary layer is an analysis of flow around an airfoil using a CFD commercia...
Runge-Kutta/Implicit methods for the solution of the Navier-Stokes equations provide superior conver...
The Backward Differentiation Formulae (BDF) of orders one to six are implemented in an in-house thre...
Abstract. Textbook multigrid efficiencies for high Reynolds number simulations based on the incom-pr...
International audienceThe aim of this work is to contribute to the understanding of sensitivity of b...
Reynolds Averaged Navier Stokes (RANS) equations are solved using third order upwind biased Roe's sc...
There is a large variety of numerical methods that are used to solve the many flow problems to which...
An efficient procedure for solving the fully linearized form of the boundary-layer equations is desc...
In order to handle turbulent flow problems, one equation turbulence models are implemented in to a p...