Cp plot for a 3d airfoil
 

Hi everybody; I would like to plot the Cp distribution over a 3d-airfoil (a centerboard) for several 2d sections; anyone knows how to do that? Thanks in advance, bye

Re: Cp plot for a 3d airfoil
 

Another thing: I know that, creating an iso-clip of the wall-surface of the centerboard at a certain value of the z-coordinate I can obtain a near-to-2D Cp Plot plotting the pressure coefficent on the clipped surface. I guess that a better method exists...

bye