Two different viscous-inviscid interaction schemes were developed for the analysis of steady, turbulent, transonic, separated flows over axisymmetric bodies. The viscous and inviscid solutions are coupled through the displacement concept using a transpiration velocity approach. In the semi-inverse interaction scheme, the viscous and inviscid equations are solved in an explicitly separate manner and the displacement thickness distribution is iteratively updated by a simple coupling algorithm. In the simultaneous interaction method, local solutions of viscous and inviscid equations are treated simultaneously, and the displacement thickness is treated as an unknown and is obtained as a part of the solution through a global iteration procedure....
The feasibility of the method of lines for solutions of physical problems requiring nonuniform grid ...
This thesis presents the development of a tool integrated in the UNS3D code, proprietary of Alenia A...
The Baldwin-Barth turbulence model was implemented into Zeta, a time-accurate, zonal, integro-differ...
An efficient and accurate method for solving the viscous shock layer equations for hypersonic flows ...
Fully elliptic forms of the transport equations have been solved numerically for two flow configurat...
An airfoil is placed in a high Reynolds number but subsonic fluid flow and is subject to very slow p...
Computations of viscous-inviscid interacting internal flowfields are presented for steady and unstea...
A new interacting boundary layer approach for computing the viscous transonic flow over airfoils is ...
Viscous transonic flows at large Reynolds numbers over 3-D wings were analyzed using a zonal viscid-...
Correlations between specific velocity and vorticity components dictate how the distributions of mea...
An approximate axisymmetric method was developed which can reliably calculate fully viscous hyperson...
The reliable prediction of turbulent non-equilibrium flows is of high academic and industrial intere...
Computational models which analyze viscous/inviscid flow processes in jet aircraft exhaust plumes ar...
Numerical simulations have been here carried out for turbulent flows in geometries relevant to elect...
Numerical simulations have been here carried out for turbulent flows in geometries relevant to elect...
The feasibility of the method of lines for solutions of physical problems requiring nonuniform grid ...
This thesis presents the development of a tool integrated in the UNS3D code, proprietary of Alenia A...
The Baldwin-Barth turbulence model was implemented into Zeta, a time-accurate, zonal, integro-differ...
An efficient and accurate method for solving the viscous shock layer equations for hypersonic flows ...
Fully elliptic forms of the transport equations have been solved numerically for two flow configurat...
An airfoil is placed in a high Reynolds number but subsonic fluid flow and is subject to very slow p...
Computations of viscous-inviscid interacting internal flowfields are presented for steady and unstea...
A new interacting boundary layer approach for computing the viscous transonic flow over airfoils is ...
Viscous transonic flows at large Reynolds numbers over 3-D wings were analyzed using a zonal viscid-...
Correlations between specific velocity and vorticity components dictate how the distributions of mea...
An approximate axisymmetric method was developed which can reliably calculate fully viscous hyperson...
The reliable prediction of turbulent non-equilibrium flows is of high academic and industrial intere...
Computational models which analyze viscous/inviscid flow processes in jet aircraft exhaust plumes ar...
Numerical simulations have been here carried out for turbulent flows in geometries relevant to elect...
Numerical simulations have been here carried out for turbulent flows in geometries relevant to elect...
The feasibility of the method of lines for solutions of physical problems requiring nonuniform grid ...
This thesis presents the development of a tool integrated in the UNS3D code, proprietary of Alenia A...
The Baldwin-Barth turbulence model was implemented into Zeta, a time-accurate, zonal, integro-differ...