Breadcrumbs Section. Click here to navigate to respective pages.
Chapter
Chapter
Boundary condition. As mentioned before two different upstream boundary conditions are used, a measured flow profile and a uniform flow profile. The boundary is divided into several sub-areas and mass-and momentum sources are applied to these sub-areas. At the downstream boundary a reference pressure and an outflow area is specified. The pressure 0 is chosen because it is an incompressible flow case and the gravity force is left out. In the 3-D calculation a logarithmic wall law with a rough extension is in the boundary layer calculation. The roughness is given as an
DOI link for Boundary condition. As mentioned before two different upstream boundary conditions are used, a measured flow profile and a uniform flow profile. The boundary is divided into several sub-areas and mass-and momentum sources are applied to these sub-areas. At the downstream boundary a reference pressure and an outflow area is specified. The pressure 0 is chosen because it is an incompressible flow case and the gravity force is left out. In the 3-D calculation a logarithmic wall law with a rough extension is in the boundary layer calculation. The roughness is given as an
Boundary condition. As mentioned before two different upstream boundary conditions are used, a measured flow profile and a uniform flow profile. The boundary is divided into several sub-areas and mass-and momentum sources are applied to these sub-areas. At the downstream boundary a reference pressure and an outflow area is specified. The pressure 0 is chosen because it is an incompressible flow case and the gravity force is left out. In the 3-D calculation a logarithmic wall law with a rough extension is in the boundary layer calculation. The roughness is given as an
ABSTRACT