Morphing wing cfd analysis in transition
I am new at this cfd issue so, i have a question.
Also, i cannot decide the prefix of the thread so i chose [other]. :(
i want to investigate a morphing wing in trasition. Is it possible?
in details, NACA 0012 airfoil is going to morph into NACA4412 in 10 seconds for example.
i want to investigate this transition case especially in terms of turbulence so i going to use LES i think.
Thanks for all of you!
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