FREQ3
Bulk Data Entry Defines a set of frequencies for the modal method of frequency response analysis by specifying the number of frequencies between modal frequencies.
Format
| (1) | (2) | (3) | (4) | (5) | (6) | (7) | (8) | (9) | (10) | 
|---|---|---|---|---|---|---|---|---|---|
| FREQ3 | SID | F1 | F2 | TYPE | NEF | CLUSTER | 
Example
| (1) | (2) | (3) | (4) | (5) | (6) | (7) | (8) | (9) | (10) | 
|---|---|---|---|---|---|---|---|---|---|
| FREQ3 | 6 | 20.0 | 200.0 | LINEAR | 10 | 2.0 | 
Definitions
| Field | Contents | SI Unit Example | 
|---|---|---|
| SID | Set identification
                                        number. No default (Integer > 0) | |
| F1 | Lower bound of modal
                                    frequency range in cycles per unit time. No default (Real ≥ 0.0 for TYPE = LINEAR; Real > 0.0 for TYPE = LOG) | |
| F2 | Upper bound of modal
                                    frequency range in cycles per unit time. Default = F1 (Real > 0.0, F2 ≥ F1) | |
| TYPE | Specifies linear or
                                    logarithmic interpolation between frequencies. 
 | |
| NEF | Number of excitation
                                    frequencies within each sub range including the end points. The
                                    first sub range is between F1 and the first
                                    modal frequency within the bounds. Intermediate sub ranges exist
                                    between each mode calculated within the bounds. The last sub
                                    range is between the last modal frequency within the bounds and
                                        F2. Default = 10 (Integer > 1) | |
| CLUSTER | Specifies cluster of
                                    the excitation frequency near the end points of the range. 5 Default = 1.0 (Real > 0.0) | 
Comments
- FREQ3 applies only to the modal method of frequency response analysis.
- FREQ3 entries must be selected in the Subcase Information section with FREQUENCY = SID.
- Since the forcing frequencies are near structural resonances, it is important that some amount of damping be specified.
- All FREQi entries with
                    the same set identification numbers will be used. Duplicate frequencies will be
                    ignored. 
                            
                         and 
                            
                         are considered duplicated if:(1) Where,- DFREQ
- User parameter with a default of 10-5 *
- The maximum and minimum excitation frequencies of the combined FREQi entries
 
- CLUSTER is used to
                    obtain better resolution near the modal frequencies where the response variation
                    is highest, in accordance with:(2) Where,
- -1 + 2(k - 1)/(NEF - 1) is a parametric coordinate between -1 and 1.
- k
- Excitation frequency number in the subrange (1,2,3,...,NEF)
- Frequency at the lower limit of the sub range. (If TYPE is LOG, then this is the logarithm of the frequency.)
- Frequency at the upper limit of the sub range. (If TYPE is LOG, then this is the logarithm of the frequency.)
- The k-th excitation frequency. (If TYPE is LOG, then this is the logarithm of the frequency.)
 CLUSTER > 1.0 provides closer spacing of excitation frequency towards the ends of the frequency range, while values of less than 1.0 provide closer spacing towards the center of the frequency range. For example, if the frequency range is between 10 and 20, NEF = 11, TYPE = "LINEAR"; then, the excitation frequencies for various values of CLUSTER would be as shown in the table below.Excitation Frequency Number CLUSTER 0.25 0.50 1.0 2.0 4.0 Excitation Frequencies in Hertz 1 -1.0 10.00 10.0 10.0 10.0 10.0 2 -0.8 12.95 11.8 11.0 10.53 10.27 3 -0.6 14.35 13.2 12.0 11.13 10.60 4 -0.4 14.87 14.2 13.0 11.84 11.02 5 -0.2 14.99 14.8 14.0 12.76 11.66 6 0.0 15.00 15.0 15.0 15.00 15.00 7 0.2 15.01 15.2 16.0 17.24 18.34 8 0.4 15.13 15.8 17.0 18.16 18.98 9 0.6 15.65 16.8 18.0 18.87 19.40 10 0.8 17.05 18.2 19.0 19.47 19.73 11 1.0 20.00 20.0 20.0 20.00 20.00 
- In design optimization, the excitation frequencies are derived from the modal frequencies computed at each design iteration.
- In modal analysis, solutions for modal degrees-of-freedom from rigid body modes at zero excitation frequencies may be discarded. Solutions for non-zero modes are retained.
- This card is represented as a load collector in HyperMesh.