July 6, 2019 at 2:20 pmsirusblack07Subscriber
I have an airfoil to which i've done a fluent analysis, I successfully imported the pressure to static structural but i couldn't find a way to do this in harmonic response. I want to study the frequency response of the wing being subject to the aerodynamic loads calculated by fluent as well as a pressure on th tip of the wing.
is there a way to do this or am I just missing something?
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