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Hi guys,
I was doing a vibration analysis on different type of beams. I will take cantilever beam as an example for the problem I faced. I chose modal analysis for this experiment. After I defined the material (Al 6061-T6) and the constraint (all fixed at one end), I run the simulation.
I went to the report tab > Frequency. I am able to retrive the natural frequency of each mode. I used these values to compare with the theoretical result which was self-calculated through formula. However there is a huge difference between the numerical result (software) and theoretical result(self-calculated). The first 2 modes does not have a big differences until the 3rd mode. All the values subsititute into the formula remained the same except for the roots value. Each modes has a different value of roots.
Value of roots
Mode Roots value
1 1.875
2 4.694
3 7.855
4 10.995
5 14.137
Is there by any chance that the roots value are different in the software? However to my knowledge, the roots value is a universal fixed value. From books to research papers, the roots value for each mode are the same. Does anyone know why will the result deviate by so much and the percentage error is more than 10%? I would like to add one more point, my theoretical result is almost the same as a similar research paper numerical result using ansys software.
I have attached the formula and results for your reference.
Thanks and appreciate any help or suggestion given!!
Solved! Go to Solution.