Hybrid RANS-LES computations of the separated flow over a wall-mounted hump are presented, which employ different grey-area mitigation techniques in the framework of a structured and an unstructured flow solver. Two zonal approaches using different synthetic-turbulence generators at the RANS-LES inter- face, as well as a non-zonal approach based on a shear-layer-adapted subgrid scale are compared in detail with validation data from a wind-tunnel experiment. Irrespective of the applied flow solver, the differ- ent methods are shown to be similarly effective in reducing the grey area compared to the basic hybrid RANS-LES model, and thus provide satisfying mean-flow predictions of the pressure-induced separation
Turbulent flows around airplane wings cannot be simulated using wall-resolved LES methods for the ne...
Xiao et al. [1] proposed an interesting hybrid LES/RANS method in which they use two solvers and sol...
International audienceWMLES simulations of a flat-plate zero-pressure-gradient boundary layer are do...
Hybrid RANS-LES computations of the separated flow over a wall-mounted hump are presented, which emp...
A study is presented evaluating the performance of zonal and non-zonal hybrid RANS-LES approaches fo...
The use of hybrid RANS-LES methods has become widespread during the last decade, as an interesting a...
Hybrid Reynolds-Average Navier-Stokes (RANS)-Large-Eddy Simulations (LES) techniques are now seen by...
This paper presents a new approach for mitigating the unphysical delay in the Reynolds-averaged Navi...
\ua9 2018 A grey area mitigation method is proposed for hybrid RANS-LES modeling. The proposed metho...
International audienceDuring the transition from the RANS (Reynolds-Averaged Navier-Stokes) mode to ...
International audienceA robust strategy for the RANS shielding of attached boundary layers in a hybr...
In order to improve turbomachinery performances it is necessary to correctly predict secondary and t...
Separation can be seen in most aerodynamic flows, but accurate prediction of separated flows is stil...
Hybrid simulations that couple the solution of the Reynolds-Averaged Navier-Stokes equations (RANS) ...
Xiao and Jenny (2012) proposed an interesting hybrid LES/RANS method in which they use two solvers a...
Turbulent flows around airplane wings cannot be simulated using wall-resolved LES methods for the ne...
Xiao et al. [1] proposed an interesting hybrid LES/RANS method in which they use two solvers and sol...
International audienceWMLES simulations of a flat-plate zero-pressure-gradient boundary layer are do...
Hybrid RANS-LES computations of the separated flow over a wall-mounted hump are presented, which emp...
A study is presented evaluating the performance of zonal and non-zonal hybrid RANS-LES approaches fo...
The use of hybrid RANS-LES methods has become widespread during the last decade, as an interesting a...
Hybrid Reynolds-Average Navier-Stokes (RANS)-Large-Eddy Simulations (LES) techniques are now seen by...
This paper presents a new approach for mitigating the unphysical delay in the Reynolds-averaged Navi...
\ua9 2018 A grey area mitigation method is proposed for hybrid RANS-LES modeling. The proposed metho...
International audienceDuring the transition from the RANS (Reynolds-Averaged Navier-Stokes) mode to ...
International audienceA robust strategy for the RANS shielding of attached boundary layers in a hybr...
In order to improve turbomachinery performances it is necessary to correctly predict secondary and t...
Separation can be seen in most aerodynamic flows, but accurate prediction of separated flows is stil...
Hybrid simulations that couple the solution of the Reynolds-Averaged Navier-Stokes equations (RANS) ...
Xiao and Jenny (2012) proposed an interesting hybrid LES/RANS method in which they use two solvers a...
Turbulent flows around airplane wings cannot be simulated using wall-resolved LES methods for the ne...
Xiao et al. [1] proposed an interesting hybrid LES/RANS method in which they use two solvers and sol...
International audienceWMLES simulations of a flat-plate zero-pressure-gradient boundary layer are do...