Command reference help topics
Laminate Sine Output Requests dialog box
Note: The laminate dynamic solver writes the frequency and peak results to binary files. To instruct the solver to also write these results to text files, set the Text Output customer default.
Tip:
To find a customer default, choose File tab→Utilities→Customer Defaults, and click Find Default .
| Modeling Object | |||||||||||
|---|---|---|---|---|---|---|---|---|---|---|---|
| Name | Sets the name for the laminate sine output requests modeling object. The name appears in the Output Requests page of the Sine Event dialog box. | ||||||||||
| Properties | |||||||||||
| The Output Request and Element Selection or Node Selection subgroups appear on all the following pages and the options are almost identical: Accelerations, Displacements, Element Forces, Grid Point Forces, MPC Forces, SPC Forces, Strains, Stresses and Velocities. | |||||||||||
| Accelerations page | |||||||||||
| Enable Accelerations Request | Computes acceleration sine results if the SOL 103 Real Eigenvalues OP2 file contains displacement results. | ||||||||||
| Displacements page | |||||||||||
| Enable Displacements Request | Computes displacement sine results if the SOL 103 Real Eigenvalues OP2 file contains displacement results. | ||||||||||
| Element Forces page | |||||||||||
| Enable Element Forces Request | Computes element force sine results if the SOL 103 Real Eigenvalues OP2 file contains element force results. | ||||||||||
| Failure Metrics page | |||||||||||
| Source for Allowables and Failure Theories | Specifies the Nastran OP2 result file for the SOL 103 Real Eigenvalues solution as the source for the material strength and failure theory properties.Note: To use different failure theories or new allowable values, you need to resolve the SOL 103 Real Eigenvalues solution after you modify its settings. | ||||||||||
| Output Frequencies | Available when Enable Homogeneous or Enable Layered is selected.Specifies the output frequencies at which the homogeneous and layered output requests are requested. You can set it to At Frequency, Peak, or At Frequency and Peak.For more information, see the Output Frequencies option in the Output Request group. | ||||||||||
| Enable Homogeneous | Computes failure metrics for elements that reference homogeneous materials at the specified output frequencies. The following Homogeneous Output Request options are available.Failure ModeSpecifies the failure mode which can be either Yield or Ultimate. The software uses the value of either yield strength or ultimate strength in the computation of the failure index and the margin of safety.Failure IndexEnables the computation of failure index results for homogenous elements using the following equation:where:F is the failure index.σVM is Von Mises stress.σall is the ultimate or yield strength property of your material. The yield and ultimate strengths are stored in the OP2 file.Margin of SafetyEnables the computation of margin of safety results for homogenous elements using the following equation:where:MS is the margin of safety.FS is the safety factor.Safety FactorSets the safety factor value that is used to compute the margin of safety.Output LocationSpecifies the location at which the software computes stress results. For more information, see the Output Location option in the Output Request group.ElementsSpecifies on which elements the software computes the output results.For more information, see the options in the Element Selection group. | where:F is the failure index.σVM is Von Mises stress.σall is the ultimate or yield strength property of your material. The yield and ultimate strengths are stored in the OP2 file. | where:MS is the margin of safety.FS is the safety factor. | ||||||||
| where:F is the failure index.σVM is Von Mises stress.σall is the ultimate or yield strength property of your material. The yield and ultimate strengths are stored in the OP2 file. | |||||||||||
| where:MS is the margin of safety.FS is the safety factor. | |||||||||||
| Enable Layered | Computes failure metric results for elements that reference a laminate physical property or a solid laminate physical property at the specified output frequencies. The following Layered Output Request options are available.Failure IndexEnables the computation of failure index results for each ply.Strength RatioEnables the computation of strength ratio results for each ply.Margin of SafetyEnables the computation of margin of safety results for each ply.Safety FactorSets the safety factor value that is used to compute the strength ratio and margin of safety.Output LocationSpecifies the location at which the software computes the strain or stress results. See the Output Location option in the Output Request group, above.ElementsSpecifies the elements on which the software computes the output results. See the options in the Element Selection group.Note: The equations for failure index, strength ratio, and margin of safety depend on the failure theory that you defined in the Laminate Modeler, Layup Modeler, or Solid Laminate Modeler dialog box. | ||||||||||
| Grid Point Forces page | |||||||||||
| Enable Grid Point Forces Request | Computes grid point force sine results if the SOL 103 Real Eigenvalues OP2 file contains grid point force results. The software can only compute at frequency and peak results for this quantity. | ||||||||||
| MPC Forces page | |||||||||||
| Enable MPC Forces Request | Computes multipoint constraint (MPC) force sine results if the SOL 103 Real Eigenvalues OP2 file contains MPC force results. | ||||||||||
| SPC Forces page | |||||||||||
| Enable SPC Forces Request | Computes single-point constraint (SPC) force sine results if the SOL 103 Real Eigenvalues OP2 file contains SPC force results. | ||||||||||
| Strains page | |||||||||||
| Enable Strains Request | Computes strain sine results if the SOL 103 Real Eigenvalues OP2 file contains strain results.Note: Laminate Dynamics computes sine ply strain results at the same locations that are used for the ply results in the SOL 103 Real Eigenvalues OP2 file. For 3D laminates, before solving your Nastran solution, you define the ply location from the Composite Solid Ply Output list on the Strain page in the Structural Output Requests dialog box. | ||||||||||
| Stresses page | |||||||||||
| Enable Stresses Request | Computes stress sine results if the SOL 103 Real Eigenvalues OP2 file contains stress results.Note: Laminate Dynamics computes sine ply stress results at the same locations that are used for the ply results in the SOL 103 Real Eigenvalues OP2 file. For 3D laminates, before solving your Nastran solution, you set the ply location from the Composite Solid Ply Output list on the Stress page in the Structural Output Requests dialog box. | ||||||||||
| Velocities page | |||||||||||
| Enable Velocities Request | Computes velocity sine results if the SOL 103 Real Eigenvalues OP2 file contains displacement results. | ||||||||||
| Complex Results page | |||||||||||
| Specifies the format of the complex results that the software writes to the output files. | |||||||||||
| Complex Output Option | Select Magnitude/Phase or Real/Imaginary.The default is Magnitude/Phase. |
Output Request options
| Output Request | |
|---|---|
| At Frequency | Enables the computation of harmonic dynamic responses for the requested result set. The responses are output as contours at each excitation frequency and are complex except for Von Mises stresses, failure indices, strength ratios, and margins of safety. |
| Peak | Enables the computation of peak values for the requested result set. Peak responses are output as contours at 0 Hz frequency and may also be identified as peak envelopes. |
| XY Functions****XY Functions for Homogeneous Elements | Not available on the Grid Point Forces page.Enables the computation of the response functions for the requested result set in the SORT2 format at the specified excitation frequencies. This allows you to plot the functions from the XY Function Navigator.The software does not output the XY functions for failure metrics, which include failure indices, strength ratios, and margins of safety. Although most response functions are written to the binary results file, some may not be supported for post-processing in the XY Function Navigator. |
| Output Location | Available on the Strains, Stresses, and Failure Metrics pages.Specifies the location at which the software computes the requested strain, stress, and failure metric results.CenterComputes the results only at the center of each element.Center and CornerComputes the results at the center and corners of each element. For example, for a hexahedral element, you get results at 9 different locations of each element. |
Element or Node Selection options
| Element Selection or Node Selection | |
|---|---|
| Elements or Nodes | Specifies the entities on which the software computes the output results. AllComputes requested results on all nodes or elements which have corresponding results in the OP2 file generated by the SOL 103 Real Eigenvalues solution.GroupComputes requested results on nodes or elements that are in the selected group. |
| Group Reference | Appears when Elements or Nodes is set to Group.Applies the requested output results to the selected group. For more information, see Group Reference options. |
| Select Object | Appears when Elements or Nodes is set to Group.Lets you select elements or nodes to request the output results on them.Excluded lets you remove individual entities from within your selected object. Note: The Element Selection Filtering options are available when the Type Filter list on the Top Border bar is set to Elements. |
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Related Topics
Laminates failure analysis
Laminate Dynamics
Laminate Sine Output Requests dialog box, Simcenter 3D 2021.1 Series
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Source: https://docs.sw.siemens.com/en-US/doc/289054037/PL20200601120302950.advanced/xid1164367 · retrieved 2026-07-17