If centrifugal loading (cf. *DLOAD) is found, it is assumed that the complete calculation (eigenmode calculation inclusive) has been performed in a relative coordinate system attached to the rotating structure. The centrifugal loading is kept fixed and is not subject to the harmonic excitation. Coriolis forces are activated for any part subject to centrifugal loading. The resulting response (displacements, stresses etc.) from the steady state calculation is in the rotating (relative) system, without the static centrifugal part.

The displacement boundary conditions in a modal dynamic analysis should match zero boundary conditions in the same nodes and same directions in the step used for the determination of the eigenmodes. They can be defined using *BOUNDARY cards or *BASE MOTION cards. The latter can also be used to define an acceleration. Temperature loading or residual stresses are not allowed. If such loading arises, the direct integration dynamics procedure should be used.

One can define loading which is shifted by by using the parameter LOAD CASE = 2 on the loading cards (e.g. *CLOAD).

The frequency range is specified by its lower and upper bound. The number of data points within this range can also be defined by the user. If no eigenvalues occur within the specified range, this is the total number of data points taken, i.e. including the lower frequency bound and the upper frequency bound. If one or more eigenvalues fall within the specified range, points are taken in between the lower frequency bound and the lowest eigenfrequency in the range, between any subsequent eigenfrequencies in the range and points in between the highest eigenfrequency in the range and the upper frequency bound. In addition, the eigenfrequencies are also included in the data points. Consequently, if eigenfrequencies belong to the specified range, data points are taken. They are equally spaced in between the fixed points (lower frequency bound, upper frequency bound and eigenfrequencies) if the user specifies a bias equal to 1. If a different bias is specified, the data points are concentrated about the fixed points.

The following damping options are available:

• Rayleigh damping by means of the *MODAL DAMPING key card. It assumes the damping matrix to be a linear combination of the problem's stiffness matrix and mass matrix. This splits the problem according to its eigenmodes, and leads to ordinary differential equations.
• Direct damping by means of the *MODAL DAMPING key card. The damping coefficient can be given for each mode separately.
• Structural damping by means of the *DAMPING key card. The structural damping is a material characteristic and has to be specified as such underneath a *MATERIAL card.
• Dashpot damping by defining dashpot elements (cf. Section 6.2.39).

For nonharmonic loading, triggered by the parameter HARMONIC=NO on the *STEADY STATE DYNAMICS card, the loading across one period is not harmonic and has to be specified in the time domain. To this end the user can specify the starting time and the final time of one period and describe the loading within this period with *AMPLITUDE cards. Default is the interval and step loading. Notice that for nonharmonic loading the *AMPLITUDE cards describe amplitude versus TIME. Internally, the nonharmonic loading is expanded into a Fourier series. The user can specify the number of terms which should be used for this expansion, default is 20. The remaining input is the same as for harmonic loading, i.e. the user specifies a frequency range, the number of data points within this range and the bias. The comments above for harmonic loading also apply here, except that, since the loading is defined in the time domain, the LOAD CASE parameter does not make sense here, i.e. LOAD CASE = 1 by default.

A steady state dynamic analysis can also be performed for a cyclic symmetric structure. To this end, the eigenmodes must have been determined for all relevant modal diameters. For a cyclic steady state dynamic analysis the following limiations apply:

1. Nonzero boundary conditions are not allowed.
2. The displacements and velocities at the start of a step must be zero.
3. Dashpot elements are not allowed.
4. Structural damping is not allowed.
5. If centrifugal forces apply, the corresponding Coriolis forces are not taken into account. The user has to assure that they are small enough so that they can be neglected.

For cyclic symmetric structures the sector used in the corresponding *FREQUENCY step is expanded into 360 and the eigenmodes are rescaled based on the mass of this expansion, i.e. they are divided by (for nodal diameter 0 and M/2, the latter only if M is even) or (other nodal diameters). M is the number of bases sectors in 360 .

The output of a steady state dynamics calculation is complex, i.e. it consists of a real and an imaginary part. Consequently, if the user saves the displacements to file, there will be two entries: first the real part of the displacement, then the imaginary part. This also applies to all other output variables such as temperature or stress. For the displacements, the temperatures and the stresses the user can request that these variables are stored as magnitude and phase (in that order) by selecting beneath the *NODE FILE card PU, PNT and PHS instead of U, NT and S respectively. This does not apply to the *NODE PRINT card.

Special caution has to be applied if 1D and 2D elements are used. Since these elements are internally expanded into 3D elements, the application of boundary conditions and point forces to nodes requires the creation of multiple point constraints linking the original nodes to their expanded counterparts. These MPC's change the structure of the stiffness and mass matrix. However, the stiffness and mass matrix is stored in the .eig file in the *FREQUENCY step preceding the *STEADY STATE DYNAMICS step. This is necessary, since the mass matrix is needed for the treatment of the initial conditions () and the stiffness matrix for taking nonzero boundary conditions into account. Summarizing, the *STEADY STATE DYNAMICS step should not introduce point loads or nonzero boundary conditions in nodes in which no point force or boundary condition was defined in the *FREQUENCY step. The value of the point force and boundary conditions in the *FREQUENCY step can be set to zero. An example for the application of point forces to shells is given in shellf.inp of the test example set.