TY - GEN
T1 - Implementation of a size field based isotropic hex core mesh algorithm
AU - Steinbrenner, John P.
AU - Wyman, Nick J.
AU - Jefferies, Mike S.
AU - Karman, Steve L.
AU - Shipman, Jeremy
N1 - Publisher Copyright:
© 2020, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.
PY - 2020
Y1 - 2020
N2 - This paper introduces an isotropic hex core meshing scheme based on a scalar function size field defined by user-defined shape primitives, boundary meshes and/or solution adaptation cloud point data. Meshing starts with a small number of root voxel elements, which are then refined via an octree framework to the size field specification. Voxel elements are classified as either cutting, inside or outside of the prescribed surface mesh, resulting in sets of elements wholly outside the surface grid boundaries (external mode) and inside any defined outer boundaries (internal mode). Voxels are then converted to hex core (tet, pyramid and hex) form, processed and finally connected to isoptropic tet cells lying between hex core and surface grid regions. Examples of hex core meshes are provided.
AB - This paper introduces an isotropic hex core meshing scheme based on a scalar function size field defined by user-defined shape primitives, boundary meshes and/or solution adaptation cloud point data. Meshing starts with a small number of root voxel elements, which are then refined via an octree framework to the size field specification. Voxel elements are classified as either cutting, inside or outside of the prescribed surface mesh, resulting in sets of elements wholly outside the surface grid boundaries (external mode) and inside any defined outer boundaries (internal mode). Voxels are then converted to hex core (tet, pyramid and hex) form, processed and finally connected to isoptropic tet cells lying between hex core and surface grid regions. Examples of hex core meshes are provided.
UR - http://www.scopus.com/inward/record.url?scp=85091313402&partnerID=8YFLogxK
U2 - 10.2514/6.2020-1408
DO - 10.2514/6.2020-1408
M3 - Conference contribution
AN - SCOPUS:85091313402
SN - 9781624105951
T3 - AIAA Scitech 2020 Forum
BT - AIAA Scitech 2020 Forum
PB - American Institute of Aeronautics and Astronautics Inc, AIAA
T2 - AIAA Scitech Forum, 2020
Y2 - 6 January 2020 through 10 January 2020
ER -