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NACA 0015 Airfoil Aerodynamics Analysis by shubham mali is a document available to read on EtoBox.
What is NACA 0015 Airfoil Aerodynamics Analysis about?
Analyze the aerodynamic behaviour of the NACA 0015 aerofoil through (CFD) simulations at different angles of attack, utilizing ANSYS Fluent software . The primary objective is to reproduce the lift and drag coefficients of the symmetrical NACA 0015 aerofoil across a range of angles (0 – 180 degrees) to gain insights into its performance characteristics.
- Author
- shubham mali
- Language
- EN