flowfield CFD REFERENCE

Mesh families and topology

Structured, unstructured and hybrid grids serve different geometric and numerical needs.

Connectivity and cell shape are separate

A structured block has logically indexed cells, often quadrilateral in 2D or hexahedral in 3D. A multiblock grid joins several such regions. An unstructured grid stores connectivity explicitly and can use tetrahedra, prisms, hexes, polyhedra or a mix. A Cartesian core is a particular arrangement of cells, and a hybrid grid can combine a prism layer with an unstructured or Cartesian core.

Family Where it helps What to inspect
Structured O-grid Wraps the body, with orderly surface-normal spacing. Trailing-edge treatment and how well the wake is resolved outside the near-body block.
Structured C-grid Wraps from a downstream cut around the airfoil and can extend a refined block into the wake. The wake cut, block interfaces and cell quality near the trailing edge.
Multiblock H-type / mixed topology Fits selected passages or larger aircraft assemblies using connected blocks. Effort to maintain quality at block joins, junctions and sharply curved surfaces.
Unstructured tet or poly core with prisms Fits complex wing-body geometry, flap gaps and assemblies. Layer collapse, size transitions, curvature and solver-specific mesh quality.
Cartesian or octree core Supports local refinement and automated grid generation. Wall representation, tiny cut cells or poor geometry conformity, depending on the method.

High aspect ratio can be useful in a boundary layer when cells align with the dominant gradients. The same stretching can be a problem in an eddy-resolving wake. Judge quality against the flow, the discretization and the wall treatment together.

Sources