# A semi-structured approach to curvilinear mesh generation around streamlined bodies

## TL;DR

This paper introduces a semi-structured high-order mesh generation method for streamlined bodies, combining structured near-field meshes with unstructured far-field meshes, optimized for high Reynolds number flow simulations.

## Contribution

The novel approach integrates medial axis partitioning, high-order meshing, and specialized treatment of critical regions to produce high-quality, anisotropic meshes suitable for complex aerodynamic simulations.

## Key findings

- Successfully applied to a NACA0012 wing model
- Produces highly stretched boundary layer elements
- Allows flexible partitioning independent of local geometry

## Abstract

We present an approach for robust high-order mesh generation specially tailored to streamlined bodies. The method is based on a semi-sructured approach which combines the high quality of structured meshes in the near-field with the flexibility of unstructured meshes in the far-field. We utilise medial axis technology to robustly partition the near-field into blocks which can be meshed coarsely with a linear swept mesher. A high-order mesh of the near-field is then generated and split using an isoparametric approach which allows us to obtain highly stretched elements aligned with the flow field. Special treatment of the partition is performed on the wing root juntion and the trailing edge --- into the wake --- to obtain an H-type mesh configuration with anisotropic hexahedra ideal for the strong shear of high Reynolds number simulations. We then proceed to discretise the far-field using traditional robust tetrahedral meshing tools. This workflow is made possible by two sets of tools: CADfix, focused on CAD system, the block partitioning of the near-field and the generation of a linear mesh; and NekMesh, focused on the curving of the high-order mesh and the generation of highly-stretched boundary layer elements. We demonstrate this approach on a NACA0012 wing attached to a wall and show that a gap between the wake partition and the wall can be inserted to remove the dependency of the partitioning procedure on the local geometry.