1. Aerodynamic Characteristics of NACA 0012 Airfoil Section at Angles of Attack from 0° to 180°;Critzos,1955
2. Summary of Airfoil Data;Abbott,1945
3. Drag reduction of flat plate normal to airstream by flow control using a rod
4. Aerodynamic Characteristics of Seven Symmetrical Airfoil Sections through 180 Degree Angle of Attack for Use in Aerodynamic Analysis of Vertical Axis Wind Turbines;Sheldahl,1981
5. Low-Speed Aerodynamic Characteristics of NACA-0012 Aerofoil Section, Including the Effects of Upper-Surface Roughness Simulating Hoar Frost;Gregory,1973