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analysis of airflow over NACA 0012 airfoil with the scope to obtain CL, CD and CL/CD for the given airfoil under these conditions
by slilbaekslilbaek
maddy112002 created this project
about 1 month ago
analysis of airflow over NACA 0012 airfoil with the scope to obtain CL, CD and CL/CD for the given airfoil under these conditions