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How to solve Laplacian equation in Converging-Diverging Nozzle

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I am right now having a 2D C-D nozzle model with a flux dphi/dx=1 pn the left boundary. I used laplace equation under PDE solver tab to solve. By setting the left boundary to flux g=1 and leave all other boundaries zero flux, I got a plot of all constant phi in the nozzle region. This is obviously not right. Can someone help me with the set up? Thanks a lot!


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