A method for the generation of hybrid prismatic/tetrahedral grids is described for complex three-dimensional geometries, including multibody domains, and employed for viscous flows around an aircraft. The prisms cover the region close to each body's surface, while tetrahedra are created elsewhere. A special method is presented that allows the generation of single-block, nonoverlapping prismatic meshes even in complex geometries that contain narrow gaps and cavities. Examples of cases treated by this method include wing-engine configurations as well as multi-element wings. The second development is a combined octree/advancing front method for the generation of the tetrahedra of the hybrid mesh.
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