The adequate representation of turbulence is crucial for the predictive accuracy of the computational method used in the turbomachinery design process. While unsteady simulations are of ever-increasing importance, steady Reynolds-Averaged Navier-Stokes computations will remain the workhorse of industrial CFD for some time. Turbulence treatments for both cases are presented. Since standard linear eddy-viscosity models exhibit some well-known deficiencies, a twofold strategy is pursued in the DLR-code TRACE: While the inclusion of turbomachineryspecific extensions to two-equation eddy-viscosity models forms the backbone of the turbulence modelling effort, Explicit Algebraic Reynolds Stress Models are currently validated for turbomachinery ...
The flow field in a transonic multistage compressor is compressible, three-dimensional and highly un...
In recent years codes that use the Navier-Stokes equations to compute aerodynamic flows have evolved...
Flow field around hypersonic vehicles is very complex and difficult to simulate. The boundary layers...
The adequate representation of turbulence is crucial for the predictive accuracy of the computationa...
The simulation quality of numerical flow simulations depends on the choice of physical modelling as ...
In order to maintain a competitive edge, the turbomachinery industry has to rely increasingly on des...
Improvements in mean flow and performances simulation in turbomachinery has brought research to focu...
Turbulent flows subjected to various kinds of unsteady disturbances were simulated using a large-edd...
Improvements in mean flow and performances simulation in turbomachinery has brought research to focu...
High fidelity simulations of three compressor cascades and a fundamental trailing edge flow are used...
Aeronautical aerodynamics is characterized by compressible flow at high Reynolds numbers. Therefore ...
In light of the Vision 2020 goals formulated by ACARE (Advisory Council for Aeronautics Research in ...
A general issue in turbomachinery flow computations is how to capture and resolve two kinds of unste...
Dramatic changes to aircraft design are on the horizon to meet ambitious efficiency and emissions ta...
The future use of eddy resolving simulations (ERS) such as Large Eddy Simulation (LES), Direct Numer...
The flow field in a transonic multistage compressor is compressible, three-dimensional and highly un...
In recent years codes that use the Navier-Stokes equations to compute aerodynamic flows have evolved...
Flow field around hypersonic vehicles is very complex and difficult to simulate. The boundary layers...
The adequate representation of turbulence is crucial for the predictive accuracy of the computationa...
The simulation quality of numerical flow simulations depends on the choice of physical modelling as ...
In order to maintain a competitive edge, the turbomachinery industry has to rely increasingly on des...
Improvements in mean flow and performances simulation in turbomachinery has brought research to focu...
Turbulent flows subjected to various kinds of unsteady disturbances were simulated using a large-edd...
Improvements in mean flow and performances simulation in turbomachinery has brought research to focu...
High fidelity simulations of three compressor cascades and a fundamental trailing edge flow are used...
Aeronautical aerodynamics is characterized by compressible flow at high Reynolds numbers. Therefore ...
In light of the Vision 2020 goals formulated by ACARE (Advisory Council for Aeronautics Research in ...
A general issue in turbomachinery flow computations is how to capture and resolve two kinds of unste...
Dramatic changes to aircraft design are on the horizon to meet ambitious efficiency and emissions ta...
The future use of eddy resolving simulations (ERS) such as Large Eddy Simulation (LES), Direct Numer...
The flow field in a transonic multistage compressor is compressible, three-dimensional and highly un...
In recent years codes that use the Navier-Stokes equations to compute aerodynamic flows have evolved...
Flow field around hypersonic vehicles is very complex and difficult to simulate. The boundary layers...