NACA 0012 Airfoil

Model ID: 14629


This model simulates the flow around an inclined NACA 0012 airfoil at different angles of attack using the SST turbulence model. The results show good agreement with the experimental lift data of Ladson and the pressure data of Gregory and O’Reilly.

Ce modèle a été construit avec les éléments suivants:

CFD Module