Eigenfrequency Analysis
An eigenfrequency study solves for the eigenfrequencies (natural frequencies) and the shapes of the corresponding eigenmodes.
When performing an eigenfrequency analysis, you can specify whether to look at the mathematically more fundamental eigenvalue, λ, or the eigenfrequency, f, which is more commonly used in a structural mechanics context. The relation between the two is
where i is the imaginary unit.
Because only the shape and not the size of the modes (eigenvectors) have physical significance, the computed modes can be scaled arbitrarily. You can select the method for scaling in the Eigenvalue Solver node of the solver sequence. If output of mass participation factors is required, then Scaling of eigenvectors must be set to Mass matrix. This means that the eigenmodes U are orthogonalized with respect to the mass matrix M so that
(2-1)
This is a common choice for the scaling of eigenvectors within the structural mechanics field.
The mass (or ‘modal’) participation factor for mode i in direction j, rij, is defined as
Here, dj is a vector containing unity displacement in all degrees of freedom representing translation in direction j. The mass participation factor gives an indication of to which extent a certain mode might respond to an excitation in that direction.
The mass participation factors have the important property that when their squares for a certain direction are summed over all modes, this sum approaches the total mass of the model:
If you use a modal superposition method to solve a forced response problem, then in practice you do not solve for all possible modes but just a limited number. This property if the mass participation factors can then be used for investigating how well a certain number of selected modes represent the total mass of the system.
The mass participation factors are available as a global variables, and these can be shown in a table using a Global Evaluation node under Derived Values in the Results branch, for example. The participation factor variables are available as predefined variables in the Solver submenu.
For an example showing how to compute modal mass, see In-Plane Framework with Discrete Mass and Mass Moment of Inertia: Application Library path Structural_Mechanics_Module/Verification_Examples/inplane_framework_freq.
For an example showing an eigenfrequency computation in a model having a rigid body mode, see Eigenfrequency Analysis of a Free Cylinder: Application Library path Structural_Mechanics_Module/Verification_Examples/free_cylinder.
In the COMSOL Multiphysics Reference Manual:
It is possible to compute eigenfrequencies for structures which are not fully constrained; this is sometimes referred to as free-free modes. For each possible rigid body mode, there is one eigenvalue which in theory is zero. The number of possible rigid body modes for different geometrical dimensions is shown in the table below.
In a piezoelectric model, one more zero eigenfrequency could appear if you have not set a reference value for the electric potential.
In practice, the natural frequencies of the rigid body modes are not computed as exactly zero, but can appear as small numbers which can even be negative or complex. If rigid body modes are present in the model, then it is important to use a nonzero value in the Search for eigenfrequencies around text field in the settings for the Eigenfrequency study step. The value should reflect the order of magnitude of the first important nonzero eigenfrequency.
Damping
If any type of damping is included in the model, an eigenfrequency solution automatically returns the damped eigenvalues. The eigenfrequencies and, in general, also the mode shapes are complex in this case. A complex-valued eigenfrequency can be interpreted so that the real part represents the actual frequency, and the imaginary part represents the damping. The ratio between the imaginary and real parts of the eigenfrequency is the relative damping of the corresponding eigenmode,
In a complex mode shape there are phase shifts between different parts of the structure, so that not all points reach the maximum at the same time under free vibration.
Some damping types will still give real valued eigenmodes, this is the case for Rayleigh damping and loss factor damping.
Prestressed Analysis
In a loaded structure, the natural frequencies may be shifted due to stress stiffening. With the Prestressed Analysis, Eigenfrequency study type you can compute eigenfrequencies taking this effect into account.