The present study is aimed at calculation of three different wall bounded two-dimensional13; turbulent flow situations, viz., fully developed flow through a plane channel, flow through a plane13; asymmetric diffuser and flow past an airfoil by solving Reynolds Averaged Navier Stokes (RANS)13; equations coupled to different eddy-viscosity based turbulence models. The turbulence models tested in13; the present study are low Reynolds number version of the k-x3B5; model of Chien [2], k-x3C9; model of Wilcox13; [11], Shear Stress Transport model of Menter [7] as a weighted combination of k-x3B5; and k-x3C9; model and13; the simplified second moment closure based k x2212;x3B5; x2212; v 2 x2212; f (so-called V2F model) model of Durbin [3].13; The ...
SIGLEAvailable from British Library Document Supply Centre-DSC:5294.937(2101) / BLDSC - British Libr...
The formulation of analytical turbulence closure models for use in computational fluid mechanics is ...
Accurate predictions of flow separation are important for aerospace design, flight accident avoidanc...
The present study is aimed at calculation of three different wall bounded two-dimensional13; turbule...
This part of the lecture first explains the limitations of the Boussinesq Eddy Viscosity hypothesis ...
The assessment of turbulence model performance in predicting flow fields that are directly relevant ...
This paper presents a computational study of the separated flow in a planer asymmetric diffuser. The...
Simulation of separated flow past an airfoil beyond stall, along with the prediction of stall itself...
The accuracy to which a turbulent boundary layer or wake can be predicted numerically depends on the...
A series of computational analyses is performed using three geometries to assess the performance of ...
Aeronautical aerodynamics is characterized by compressible flow at high Reynolds numbers. Therefore ...
The Boussinesq eddy viscosity assumption (1872) is still widely used in turbulence modeling although...
A turbulence model study was performed for the wing–body configuration of NASA’s common research mod...
This work assesses the performance of two single-equation eddy viscosity transport models that are b...
The objective of this research work is to assess the capability of the lagged eddy viscosity model i...
SIGLEAvailable from British Library Document Supply Centre-DSC:5294.937(2101) / BLDSC - British Libr...
The formulation of analytical turbulence closure models for use in computational fluid mechanics is ...
Accurate predictions of flow separation are important for aerospace design, flight accident avoidanc...
The present study is aimed at calculation of three different wall bounded two-dimensional13; turbule...
This part of the lecture first explains the limitations of the Boussinesq Eddy Viscosity hypothesis ...
The assessment of turbulence model performance in predicting flow fields that are directly relevant ...
This paper presents a computational study of the separated flow in a planer asymmetric diffuser. The...
Simulation of separated flow past an airfoil beyond stall, along with the prediction of stall itself...
The accuracy to which a turbulent boundary layer or wake can be predicted numerically depends on the...
A series of computational analyses is performed using three geometries to assess the performance of ...
Aeronautical aerodynamics is characterized by compressible flow at high Reynolds numbers. Therefore ...
The Boussinesq eddy viscosity assumption (1872) is still widely used in turbulence modeling although...
A turbulence model study was performed for the wing–body configuration of NASA’s common research mod...
This work assesses the performance of two single-equation eddy viscosity transport models that are b...
The objective of this research work is to assess the capability of the lagged eddy viscosity model i...
SIGLEAvailable from British Library Document Supply Centre-DSC:5294.937(2101) / BLDSC - British Libr...
The formulation of analytical turbulence closure models for use in computational fluid mechanics is ...
Accurate predictions of flow separation are important for aerospace design, flight accident avoidanc...