Solutions of the Favre-averaged Navier-Stokes equations for two well-documented transonic turbulent flows are compared in detail with existing experimental data. While the boundary layer in the first case remains attached, a region of extensive flow separation has been observed in the second case. Two recently developed k-epsilon, two-equation, eddy-viscosity models are used to model the turbulence field. These models satisfy the realizability constraints of the Reynolds stresses. Comparisons with the measurements are made for the wall pressure distribution, the mean streamwise velocity profiles, and turbulent quantities. Reasonably good agreement is obtained with the experimental data
The ability of two-equation models to accurately predict separated flows is analyzed from a combined...
This paper reports the wall-resolved large eddy simulations of shock-induced boundary layer separati...
Numerical solutions of the complete, time-averaged conservation equations using several eddy-viscosi...
Solutions of the time-dependent, mass-averaged Navier-Stokes equations are compared In detail with e...
A review is made of the performance of a variety of turbulence models in the evaluation of a particu...
A mathematically simple, turbulence closure model designed to treat transonic airfoil flows even wit...
A numerical investigation of transonic turbulent flows separated by curvature and shock wave - bound...
Navier-Stokes transonic airfoil calculations based on a recently developed nonequilibrium, turbulenc...
During the past five years, numerous pioneering archival publications have appeared that have presen...
A numerical study of incompressible turbulent separated flows is carried out by using two-equation t...
In recent years codes that use the Navier-Stokes equations to compute aerodynamic flows have evolved...
Results of computer code time dependent solutions of the two dimensional compressible Navier-Stokes ...
Additional results about the wing-body of the NASA Common Research Model at flight conditions derive...
Progress in modeling external aerodynamic flows achieved by using computations and experiments desig...
Two new versions of the k-omega two-equation turbulence model will be presented. The new Baseline (B...
The ability of two-equation models to accurately predict separated flows is analyzed from a combined...
This paper reports the wall-resolved large eddy simulations of shock-induced boundary layer separati...
Numerical solutions of the complete, time-averaged conservation equations using several eddy-viscosi...
Solutions of the time-dependent, mass-averaged Navier-Stokes equations are compared In detail with e...
A review is made of the performance of a variety of turbulence models in the evaluation of a particu...
A mathematically simple, turbulence closure model designed to treat transonic airfoil flows even wit...
A numerical investigation of transonic turbulent flows separated by curvature and shock wave - bound...
Navier-Stokes transonic airfoil calculations based on a recently developed nonequilibrium, turbulenc...
During the past five years, numerous pioneering archival publications have appeared that have presen...
A numerical study of incompressible turbulent separated flows is carried out by using two-equation t...
In recent years codes that use the Navier-Stokes equations to compute aerodynamic flows have evolved...
Results of computer code time dependent solutions of the two dimensional compressible Navier-Stokes ...
Additional results about the wing-body of the NASA Common Research Model at flight conditions derive...
Progress in modeling external aerodynamic flows achieved by using computations and experiments desig...
Two new versions of the k-omega two-equation turbulence model will be presented. The new Baseline (B...
The ability of two-equation models to accurately predict separated flows is analyzed from a combined...
This paper reports the wall-resolved large eddy simulations of shock-induced boundary layer separati...
Numerical solutions of the complete, time-averaged conservation equations using several eddy-viscosi...