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Flow Around an Inclined NACA 0012 Airfoil

Application 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.

Questo modello è stato realizzato con:

CFD Module

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