The influence of turbulence model and numerical technique on RANS computations is discussed in the case of turbulent boundary layer flow on a flat plate. In particular, results are presented for a centered scheme with artificial dissipation and a ENO-type scheme with the Baldwin-Lomax and Spalart-Allmaras models. First, in an a priori analysis, the truncation errors are evaluated under the assumption of parallel Couette flow, and some conclusions about mesh optimization and scheme performance are drawn. Then, the a posteriori analysis for the numerical solution of turbulent boundary, layer on a flat plate is performed. Grid Convergence Index and convergence rate analysis confirm the a priori results
Turbulent boundary layers on a flat plate configuration are simulated using synthetic turbulence gen...
The generation of a fully turbulent boundary layer profile is investigated using analytical and nume...
Key words: Wall function, RANS turbulence modelling, boundary layer approximation, sepa-ration Abstr...
The accuracy of numerical solutions for the incompressible turbulent boundary layer past a flat plat...
Accuracy of numerical solution is of paramount importance for any CFD simulation. The error in satis...
The calculation of the turbulent boundary layer is performed when a steady flow of a viscous fluid ...
Reynolds Averaged Navier Stokes (RANS) equations are solved using third order upwind biased Roe's sc...
AbstrAct: The present work is primarily concerned with studying the effects of artificial dissipatio...
Computation of Airfoil boundary layer is an analysis of flow around an airfoil using a CFD commercia...
Im Bereich der industriellen Aerodynamik stellen die Reynolds–gemittelten Navier–Stokes (RANS) Metho...
ABSTRACT: The present work is primarily concerned with studying the effects of artificial dissipatio...
A Finite Element numerical method has been developed to simulate the fluid flow over two dimensional...
A detailed grid convergence study has been conducted to establish accurate reference solutions corre...
Turbulent flows are investigated using numerical simulations. Three aspects of turbulent flows are t...
A zero pressure gradient (ZPG) boundary layer in a wind-tunnel test section was computed using two-d...
Turbulent boundary layers on a flat plate configuration are simulated using synthetic turbulence gen...
The generation of a fully turbulent boundary layer profile is investigated using analytical and nume...
Key words: Wall function, RANS turbulence modelling, boundary layer approximation, sepa-ration Abstr...
The accuracy of numerical solutions for the incompressible turbulent boundary layer past a flat plat...
Accuracy of numerical solution is of paramount importance for any CFD simulation. The error in satis...
The calculation of the turbulent boundary layer is performed when a steady flow of a viscous fluid ...
Reynolds Averaged Navier Stokes (RANS) equations are solved using third order upwind biased Roe's sc...
AbstrAct: The present work is primarily concerned with studying the effects of artificial dissipatio...
Computation of Airfoil boundary layer is an analysis of flow around an airfoil using a CFD commercia...
Im Bereich der industriellen Aerodynamik stellen die Reynolds–gemittelten Navier–Stokes (RANS) Metho...
ABSTRACT: The present work is primarily concerned with studying the effects of artificial dissipatio...
A Finite Element numerical method has been developed to simulate the fluid flow over two dimensional...
A detailed grid convergence study has been conducted to establish accurate reference solutions corre...
Turbulent flows are investigated using numerical simulations. Three aspects of turbulent flows are t...
A zero pressure gradient (ZPG) boundary layer in a wind-tunnel test section was computed using two-d...
Turbulent boundary layers on a flat plate configuration are simulated using synthetic turbulence gen...
The generation of a fully turbulent boundary layer profile is investigated using analytical and nume...
Key words: Wall function, RANS turbulence modelling, boundary layer approximation, sepa-ration Abstr...