NACA 4412 Analysis

The NACA4412 airfoil is a widely used symmetrical airfoil that has a thickness-to-chord ratio of 12% and is commonly used in the design of aircraft wings. This airfoil was developed by the National Advisory Committee for Aeronautics (NACA) during the 1930s and was used extensively in World War II fighter planes. The airfoil has a flat bottom and a curved upper surface, which creates lift when air flows over it. One of the key benefits of the NACA 4412 airfoil is its high maximum lift coefficient, which makes it suitable for use in aircraft with high lift requirements, such as military transport planes and cargo planes.