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April 19, 2024 at 7:09 pmByron NgSubscriber
I am running a simulation of two airfoils on top of each other and I cant get my lift force or scaled residulas to converge. When I change the outlet to only half of the back wall it works but when the outlet is the entire wall it doesn't work. I have na inlet velocity of 13 m/s in the x direction only.
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April 19, 2024 at 7:24 pm
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April 22, 2024 at 10:44 amRobForum Moderator
Please post some contours etc to show what the flow is doing. You can't rely on just a single line to diagnose flow.Â
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