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Skin Friction Coefficient plot over the suction side of an airfoil

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Old   October 14, 2019, 13:41
Default Skin Friction Coefficient plot over the suction side of an airfoil
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Mario
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Hello everyone,

i'm simulating a flow over a Naca-6 series airfoil and i need to plot the skin friction coefficient (Cf) at a certain timestep over the suction side of my airfoil, once having the datas for the wallShearStress obtained through the nameofthesolver -postProcess -func tool, but i'm having troubles with that.

Is there a way to do it with Paraview or a script that takes into account the change of normals along the ss of the airfoil?

Any help would be kindly accepted.
Thank you in advance.
Mario
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Old   October 15, 2019, 05:58
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Tom Fahner
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Hi Mario,

You can use the Generate Surface Normals filter to get the normals of the surface and than use a calculator to get the dot product (v1.v2 button) of the Normal vector and the wallShearStress vector.

Hope this helps,
Tom
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Old   October 15, 2019, 09:55
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Thank you Tom!
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