For creating new mesh with snappyHexMesh it is recommended to create new OpenFOAM test case just with system and constant directory and with empty directory 0. Go to your user directory and create directories for the stator region.
cd $WM_PROJECT_USER_DIR/run mkdir -p turbomachinery-CFD/meshFactory/as1/stator cd turbomachinery-CFD/meshFactory/as1/stator cp -r $WM_PROJECT_INST_DIR/Turbomachinery-CFD-XX.XX/ /tutorials/meshFactory/as1/stator/* ./
The input .STL files are located in constant/triSurface and can be directly viewed in paraview.
paraview
In this case, the interface between stator and rotor part is divided into the 36 radial strips (individual .STL files) to allow Mixing Plane averaging. (Compare to radial cases, where the rings were created on existing mesh using topoSet and createPatch). This approach was chosen just for practising purposes. Of course both approaches of creating Mixing Plane patches are possible. Following files will be used:
StatorAMI1.stl
StatorAMI2.stl
StatorHub.stl
StatorIn.stl
StatorBlade.stl
StatorShroud.stl
StatorMXP_0.stl
StatorMXP_35.stl
The initial idea is to have following mesh boundaries in the end:
stator_outlet_0
stator_outlet_35
stator_inlet
stator_hub
stator_shroud
stator_blade
stator_cyc_l
stator_cyc_r
Their number and names can change during the creation process.