This paper presents a grid and flow adaptive wall-function method for RANS turbulence modelling with emphasis on aerodynamic flows. A near-wall grid adaptation technique ensures a locally appropriate resolution depending on both the near-wall flow physics to be captured and the range of validity of the wall-function model. The near-wall RANS solutions of the Spalart-Allmaras and SST k-omega turbulence model are investigated near stagnation points and subsequent not yet fully developed turbulent flow, and in regions of adverse pressure gradient before separation. These are compared with the corresponding turbulence model specific universal wall-functions and suggestions for the design of wall-function methods for non-equilibrium ...
The Spalart-Allmaras (SA) is one of the most popular turbulence models in the aerospace CFD communit...
International audienceTo assert the validity of the wall law approach in a RANS code, systematic com...
A novel wall function formulation for Spalart-Allmaras and k-! model derived for the ow over a at ...
This report is dedicated to a new wall-function approach for RANS turbulence modelling of subsonic a...
A universal wall-function method for RANS turbulence modelling is presented, which is designed by co...
Key words: Wall function, RANS turbulence modelling, boundary layer approximation, sepa-ration Abstr...
The numerical solution of the Reynolds averaged Navier-Stokes (RANS) equations for aerodynamic flows...
A universal wall-function method for RANS turbulence modelling is presented which allows for a consi...
International audienceThe scope of this paper is to determine an optimal mesh adaptation strategy to...
A model-consistent universal wall-function method for RANS turbulence modelling is presented, which...
Accurately capturing of turbulence has been a challenging problem for both the academic study and in...
This thesis presents two new numerical wall models for computing Reynolds-Averaged-Navier-Stokes (RA...
A common alternative to full resolution of the near-wall region in computational fluid dynamics (CFD...
This paper considers grid-adaptation techniques for the boundary-layer region of hybrid meshes, wh...
Spalart-Allmaras (SA) model is a low Reynolds number (Re) model, which means that the first off-wall...
The Spalart-Allmaras (SA) is one of the most popular turbulence models in the aerospace CFD communit...
International audienceTo assert the validity of the wall law approach in a RANS code, systematic com...
A novel wall function formulation for Spalart-Allmaras and k-! model derived for the ow over a at ...
This report is dedicated to a new wall-function approach for RANS turbulence modelling of subsonic a...
A universal wall-function method for RANS turbulence modelling is presented, which is designed by co...
Key words: Wall function, RANS turbulence modelling, boundary layer approximation, sepa-ration Abstr...
The numerical solution of the Reynolds averaged Navier-Stokes (RANS) equations for aerodynamic flows...
A universal wall-function method for RANS turbulence modelling is presented which allows for a consi...
International audienceThe scope of this paper is to determine an optimal mesh adaptation strategy to...
A model-consistent universal wall-function method for RANS turbulence modelling is presented, which...
Accurately capturing of turbulence has been a challenging problem for both the academic study and in...
This thesis presents two new numerical wall models for computing Reynolds-Averaged-Navier-Stokes (RA...
A common alternative to full resolution of the near-wall region in computational fluid dynamics (CFD...
This paper considers grid-adaptation techniques for the boundary-layer region of hybrid meshes, wh...
Spalart-Allmaras (SA) model is a low Reynolds number (Re) model, which means that the first off-wall...
The Spalart-Allmaras (SA) is one of the most popular turbulence models in the aerospace CFD communit...
International audienceTo assert the validity of the wall law approach in a RANS code, systematic com...
A novel wall function formulation for Spalart-Allmaras and k-! model derived for the ow over a at ...