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Tag Archives: hybrid mesh
No one generates a mesh just to generate a mesh. The proof of a mesh’s suitability is successful use in a CFD simulation. That success can be predicated on many factors including the availability of a broad range of mesh … Continue reading
There’s a lot of good reading and listening in this week’s CFD news starting with a new CFD podcast, a proposal for sustainable research software, and the first in a series on AI and CFD. Think Before You Compute, good … Continue reading
In this new on-demand webinar we demonstrate how to generate a hybrid hexahedral-tetrahedral mesh for the Potsdam Propeller. You’ll see both approaches (solid meshing and fault tolerance meshing) to generating surface meshes on the geometry model, the T-Rex technique for … Continue reading
The SU2 team and Pointwise recently teamed up and ran one of the meshes generated for the AIAA High Lift Prediction Workshop using the latest release of SU2. Information regarding the workshop, the meshing process, solver setup, and the SU2 … Continue reading
Approaches to discretizing models for physics-based simulation have matured considerably over the years with several meshing techniques from which to choose including: multi-block structured, overset, octree, advancing front, and so on. Each of these approaches has its benefits and drawbacks when comparing one with another. Convergence and solution accuracy are evaluated among three mesh configurations of an ONERA M6 wing to help determine whether there exist any advantages of using an unstructured mixed-cell meshing approach over other unstructured advancing front and multi-block structured options. Continue reading