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Airfoil CFD - Project 1
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0 Geometries 0 Meshes 0 Simulation setups 0 ResultsAbout this project
In this project, a 2D model of a NACA 2412 airfoil is used to simulate incompressible airflow under steady-state conditions. The simulation is performed using SimScale, where a flow domain is created around the airfoil to represent real atmospheric conditions. Multiple simulations are conducted at different angles of attack (0°, 5°, 10°, and 15°) to observe the effect on pressure distribution, velocity fields, and overall aerodynamic performance. The results are analyzed through contour plots and streamlines to visualize airflow behavior.
