Abstract The goal of this paper is to implement an accurate and robust solver for compressible Navier-Stokes equations coupled with the Spalart–Allmaras model, which possesses the capability of shock-capturing and predication of boundary layer and separated flow. In a given stencil width, a WENO-Z scheme equipped with Roe flux difference split method is used to calculate the inviscid flux, and central differencing scheme for the viscous terms are employed. The explicit Runge-Kutta is adopted for the temporal discretization. The simulation results of selected cases are given to verify the validation of the solver
AbstrAct: The present work is primarily concerned with studying the effects of artificial dissipatio...
In a series of papers, Olsson (1994, 1995), Olsson & Oliger (1994), Strand (1994), Gerritsen Olsson ...
When high Reynolds turbulent flows are combined with complex and large size geometries, computers ar...
In this paper the artificial compressibility flux Discontinuous Galerkin (DG) method for the solutio...
A mixed algorithm of central and upwind difference scheme for the solution of steady/unsteady incomp...
We present a practical approach for the numerical solution of the Reynolds averaged Navier-Stokes (R...
An unstructured explicit, Reynolds averaged Navier-Stokes solver is developed to operate on inviscid...
International audienceThe majority of fluid flows that are interesting from a practical point of view ...
A stable high-order numerical scheme for direct numerical simulation (DNS) of shock-free compressibl...
The paper provides the details of the implementation and testing of the Spalart-Allmaras model of tu...
The present thesis describes the development of a computational method for the numerical simulation ...
ABSTRACT: The present work is primarily concerned with studying the effects of artificial dissipatio...
Nowadays, in spite of disadvantages of turbulence closure models for RANS (Reynolds Averaged Navier-...
This report outlines the development of a general purpose aerodynamic solver for compressible turbul...
Purpose – To develop a high-order compact finite-difference method for solving flow problems contain...
AbstrAct: The present work is primarily concerned with studying the effects of artificial dissipatio...
In a series of papers, Olsson (1994, 1995), Olsson & Oliger (1994), Strand (1994), Gerritsen Olsson ...
When high Reynolds turbulent flows are combined with complex and large size geometries, computers ar...
In this paper the artificial compressibility flux Discontinuous Galerkin (DG) method for the solutio...
A mixed algorithm of central and upwind difference scheme for the solution of steady/unsteady incomp...
We present a practical approach for the numerical solution of the Reynolds averaged Navier-Stokes (R...
An unstructured explicit, Reynolds averaged Navier-Stokes solver is developed to operate on inviscid...
International audienceThe majority of fluid flows that are interesting from a practical point of view ...
A stable high-order numerical scheme for direct numerical simulation (DNS) of shock-free compressibl...
The paper provides the details of the implementation and testing of the Spalart-Allmaras model of tu...
The present thesis describes the development of a computational method for the numerical simulation ...
ABSTRACT: The present work is primarily concerned with studying the effects of artificial dissipatio...
Nowadays, in spite of disadvantages of turbulence closure models for RANS (Reynolds Averaged Navier-...
This report outlines the development of a general purpose aerodynamic solver for compressible turbul...
Purpose – To develop a high-order compact finite-difference method for solving flow problems contain...
AbstrAct: The present work is primarily concerned with studying the effects of artificial dissipatio...
In a series of papers, Olsson (1994, 1995), Olsson & Oliger (1994), Strand (1994), Gerritsen Olsson ...
When high Reynolds turbulent flows are combined with complex and large size geometries, computers ar...