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Naca 2421 CFD Term Paper by Million Gonfa is a document available to read on EtoBox.

This study analyzes the aerodynamic performance of a NACA 2421 airfoil using CFD in ANSYS Fluent at angles of attack of 8° and 10°. The results indicate that lift increases with angle of attack and drag rises moderately, demonstrating the effectiveness of CFD for predicting airfoil performance. Overall, the research highlights the importance of CFD in understanding airflow and enhancing aircraft design.

Author

Million Gonfa

Language

EN