How can I get pressure distribution along airfoil surface?
How to write sampleDict with that I can get the pressure distribution along the airfoil?
I'm having the same problem; mine is to plot over a circular cylinder.
I searched the forum and found this
reply #5 suggested a way. I tried it once but due to some certain reasons it failed. You can have a try. If you succeed, please teach me!
You can use "sampleDict" to extract pressure data on the surface, and plot using any tool like xmgrace, python.
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