Antoli --
You can indeed do this by natural frequency (modal) analysis. If you know (or can determine) the gain of your booster Gb, then the input amplitude to the sonotrode Uinput is 20um*Gb. For the following example, assume Gb = 1.5 so Uinput = 30um.
With the above information you can run a modal analysis of the sonotrode alone. (Depending on your circumstance you may want to include the booster. However, this is usually not needed unless you are concerned with the booster's isolation mount or unless you don't know the booster's gain.)
After you run the modal analysis, when you display the desired modeshape you will see the relative amplitudes. Rotate the model until you can see the center point where the booster would attach (generally the center of the sonotrode's input face). Right click on this node and then choose Inquire\Results. Record the displacement value in the direction of the booster's axis (i.e., in the direction of the input amplitude to the sonotrode). For example, if the booster's axis would be in the Z direction, then record DZ. This displacement is the reference displacement to which all others will be compared. For the following example, assume that this value is 13.6 (your value will be different).
Now you can compute the relative amplitudes at any other location on the sonotrode. For example, at the center of the sonotrode's output surface (the face) you may click and find a DZ value of 67.2. Then this location has a relative amplitude of 67.2/13.6 = 4.94. The actual amplitude will be 20um*1.5*4.94 = 148um (i.e., 20um transducer output * booster gain * sonotrode relative amplitude). If the sonotrode is symmetric then the transverse displacements at the center of the sonotrode's face will be small.
You can use this same method for any other location on the sonotrode. For example, at a corner you might have:
DZ = 58.3 ==> relative amplitude = 58.3/13.6 = 4.29 ==> 129 microns
DX = 4.7 ==> relative amplitude = 4.7/13.6 = .346 ==> 10.4 microns
DY = 5.2 ==> relative amplitude = 5.2/13.6 = .346 ==> 11.5 microns
You may want to make the following interface settings:
1. Set the "Results options" to "Absolute value". This will then typically display a dark color at the node(s) so that the node(s) can easily be located.
If you need the stresses then you will have to also run a frequency response analysis after the modal analysis.
Don Culp
www.krell-engineering.com