Rapid meshing of turbomachinery rows using semi-unstructured multi-block conformal grids
A semi-unstructured grid generation method especially tailored for the meshing of turbomachinery blade passages and their associated cavities is presented. The method is based on a smart combination of quasi-3D methods, an ad hoc block decomposition of the domain and a grid-based solid-model-less reconstruction of the computational domain.
turbomachinery semi-unstructured grid hybrid delaunay