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Old   April 28, 2006, 08:10
Default Polyline Plots
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I solved NACA profile which is 3-D. in the X-Direction (longitudinal) I created a sereis of points along the Z-direction so I can obtain the velocity from the surface of the airfoil to the top of the domain,I have used polyline to extract the velocities for each line along the X-direction. I am not sure how to plot this velocities back on the airfoil, can someone please tell me how if it is possible ?
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