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November 20, 2023 at 8:43 am
Giorgio Casulli
SubscriberI'm studying the laminar flow on a NACA 4412 profile and I was wondering which is the critical reynolds number for this case, in particular i would like to know which is the max reynolds number at which the laminar model is able to give reliable results.
Any ideas?
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November 21, 2023 at 3:04 pm
Rob
Forum ModeratorWe can't really answer that. Flow separation, mesh, time step size, wing shape etc will all play a role, so it's not a case of giving a single value.
If you run the laminar model at what point don't you get data that agree with publications?Â
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