Abstract: A numerical model for turbulent three-dimensional flows at high Reynolds numbers is considered. The RANS approach based on the turbulence model of Spalart and Allmaras (SA) is used. The method of wall functions for modeling surface friction is implemented. Specifics of the numerical algorithm based on the LU-SGS–GMRES solver, and program implementation of the present numerical model are discussed. Numerical solutions of the compressible viscous gas flow over a flat plate and in an asymmetric diffuser, and also mathematical modeling of the turbulent mixture layer of two compressible flows are carried out to perform verification and validation of the RANS equations with the SA model for turbulence and the method of wall f...
This paper presents a grid and flow adaptive wall-function method for RANS turbulence modelling wi...
Many fluid flow applications that exist in engineering practice can be solved by means of numerical ...
A three-stage Runge-Kutta (RK) scheme with multigrid and an implicit preconditioner has been shown t...
Accurately capturing of turbulence has been a challenging problem for both the academic study and in...
Spalart-Allmaras (SA) model is a low Reynolds number (Re) model, which means that the first off-wall...
When high Reynolds turbulent flows are combined with complex and large size geometries, computers ar...
The Spalart-Allmaras (SA) is one of the most popular turbulence models in the aerospace CFD communit...
Abstract: The paper is devoted to a numerical study of the flow around spacecraft model us...
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...
A study is conducted to perform Reynolds-averaged Navier?Stokes (RANS) simulations for hypersonic fl...
In this paper the artificial compressibility flux Discontinuous Galerkin (DG) method for the solutio...
The Spalart and Allmaras turbulence model has been implemented in a numerical code to study the comp...
The work deals with the numerical solution of 3D turbulent stratified flows in atmospheric boundary ...
Thesis: S.M. in Naval Architecture and Marine Engineering; and S.M. in Mechanical Engineering , Mas...
This paper presents a grid and flow adaptive wall-function method for RANS turbulence modelling wi...
Many fluid flow applications that exist in engineering practice can be solved by means of numerical ...
A three-stage Runge-Kutta (RK) scheme with multigrid and an implicit preconditioner has been shown t...
Accurately capturing of turbulence has been a challenging problem for both the academic study and in...
Spalart-Allmaras (SA) model is a low Reynolds number (Re) model, which means that the first off-wall...
When high Reynolds turbulent flows are combined with complex and large size geometries, computers ar...
The Spalart-Allmaras (SA) is one of the most popular turbulence models in the aerospace CFD communit...
Abstract: The paper is devoted to a numerical study of the flow around spacecraft model us...
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...
A study is conducted to perform Reynolds-averaged Navier?Stokes (RANS) simulations for hypersonic fl...
In this paper the artificial compressibility flux Discontinuous Galerkin (DG) method for the solutio...
The Spalart and Allmaras turbulence model has been implemented in a numerical code to study the comp...
The work deals with the numerical solution of 3D turbulent stratified flows in atmospheric boundary ...
Thesis: S.M. in Naval Architecture and Marine Engineering; and S.M. in Mechanical Engineering , Mas...
This paper presents a grid and flow adaptive wall-function method for RANS turbulence modelling wi...
Many fluid flow applications that exist in engineering practice can be solved by means of numerical ...
A three-stage Runge-Kutta (RK) scheme with multigrid and an implicit preconditioner has been shown t...