Thirty-five airfoil boundary points can be mapped to a dense CFD mesh point cloud by a three-layer network trained with Chamfer and repulsion losses.
A parallel parameterized level set topology opti- mization framework for large-scale structures with unstructured meshes
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Loop2Net: Data-Driven Generation and Optimization of Airfoil CFD Meshes from Sparse Boundary Coordinates
Thirty-five airfoil boundary points can be mapped to a dense CFD mesh point cloud by a three-layer network trained with Chamfer and repulsion losses.