TCAE CAA analysis of NACA0012
The mesh model used has eight boundary layers created with TCAE's SnappyHexMesh.
Comprehensive engineering simulation software with unlimited licensing This article introduces CAA analysis of NACA airfoils using TCAE. This project focuses on the NACA 0012 airfoil BANCIIIc3 benchmark [1] (3D code: 0.4[m], span: 10%) and delves into the field of computational aeroacoustics (CAA). By adopting advanced techniques such as acoustic analogy and Ffowcs Williams-Hawkings, we explore unsteady simulations with a physical time of 1[s] through finite volume CFD simulations in a cell-centered framework. *For more detailed information, you can view it through the related links. For more details, please download the PDF or feel free to contact us.*
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