Aerodynamic characteristics of NACA 0012 airfoil section at angles of attack from 0 degrees to 180 degrees

Aerodynamic characteristics of NACA 0012 airfoil section at angles of attack from 0 degrees to 180 degrees

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Hauptverfasser: Critzos, Chris C, Heyson, Harry H, Boswinkle, Robert W, Jr
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creator Critzos, Chris C
Heyson, Harry H
Boswinkle, Robert W, Jr
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title Aerodynamic characteristics of NACA 0012 airfoil section at angles of attack from 0 degrees to 180 degrees
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