naca0012
Here are 7 public repositories matching this topic...
ANN based Surrogate model optimization of airfoil using XFOIL
-
Updated
Aug 4, 2025 - Jupyter Notebook
A Python-based 2D CFD solver for the Euler equations using a structured O-type grid. Capable of simulating flow around airfoils in subsonic, transonic, and supersonic regimes.
-
Updated
Dec 19, 2024 - Python
Aerospace CFD verification workflow using OpenFOAM for NACA 0012 airfoil analysis, mesh refinement and CL/CD convergence assessment.
-
Updated
May 14, 2026 - Python
2D CFD simulation of NACA0012 at 5° AoA using SST k-ω model. Mesh convergence included.
-
Updated
May 21, 2025
Improve this page
Add a description, image, and links to the naca0012 topic page so that developers can more easily learn about it.
Add this topic to your repo
To associate your repository with the naca0012 topic, visit your repo's landing page and select "manage topics."