The provided data represents Computational Fluid Dynamics (CFD) simulation results for six different airfoil shapes: NACA 0012, NACA 0015, NACA 0021, NACA 2412, NACA 2415, and NACA 4412. The data is obtained from a dataset containing CFD results for various airfoil configurations.

The dataset is organized in a CSV format. The dataset contains the following columns:

p: Pressure coefficient (Cp) values. U:0, U:1, U:2: Velocity components in three-dimensional space. Points:0, Points:1, Points:2: Coordinates of points on the airfoil.