Hi, I have done a tutorial by SimCafe Cornell namely Modal Analysis of 3d NACA 0012 Airfoil using ANSYS.
I have observed that Frequencies of vibration and their respective mass participations do not change considerably if number of mesh elements increases. (Attach pictures shows comparison between 2000 and 8000 mesh elements)
Question: Can we say that Modal Analysis is always mesh independent or its result does not change considerably upon increasing mesh elements? Waiting for answer.