[chandra shekhar pant]

Hello Foamers,
I tried to simulate a 3D NACA aerofoil in OpenFOAM. I want the velocity profile at different section of this aerofoil. To do that I need to average the velocity field in the span wise direction and then plot the velocity at different locations of the aerofoil. In the given figures: figure1 I have shown the 3D section of the aerofoil and to explicitly show what I mean by the span-wise direction; figure 2 is the contour plot of the 2D slice of the aerofoil in which I want to plot the velocity along a normal line to the surface of the aerofoil. So effectively I want to plot a velocity profile at a fixed location of aerofoil which is averaged in the spanwise direction. Is that can be processed through any OpenFOAM utility, any suggestion or comments?