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NACA 0012 Airfoil: Convective Heat Transfer Analysis
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1 Geometry 1 Mesh 1 Simulation setup 0 ResultsAbout this project
Comparative study of airflow and heat transfer over a NACA 0012 airfoil at 10 m/s, 20 m/s, and 30 m/s. Ambient temperature 300 K, Wing surface 350 K.
