The following data is provided to replicate the results: NACA-6 and NACA-4 airfoil coordinates (with 5% width fraction), CFD background and volume mesh configuration files, and FEM volume mesh configu
This case has been developed as is part of the exaFOAM project that aims to enable the open-source CFD software OpenFOAM to exploit massively parallel HPC architectures and overcome performance scalin
Upload of the numerical solutions for the Reference plane of the MONNALISA Project. Please, refer to the README file of this folder and to the articles associated.
