• Response spectrum analysis is a technique used to estimate the maximum response of a structure for a transient event. The time-history of the responses are not available. RSA is a simple and computationally inexpensive method to provide a peak response approximation, compared to conventional transient analysis.
  
• The solution is supported using four modal combination methods namely Absolute sum (ABS), Square root of sum of squares (SRSS), Navy research Laboratory's SRSS (NRL) and Complete quadratic combination (CQC). The solution requires linking to a modal analysis, which requires and uses most of the computational effort to obtain enough modes to represent the entire frequency range of input excitation and resulting response.
  

• Neuber stresses/strains can be obtained by running linear structural analysis and Neuber correction can be used to evaluate approximate local plasticity. This method is computationally inexpensive as Neuber stresses/strains are output without running a full-fledged nonline aranalysis. To successfully output Neuber results, material stress-strain curves are required to be input.
  
• The Neuber method corrects elastic results to capture any local plasticity. It is used to convert elastic stress/strain into real stress/strain when plastic deformation occurs. To apply Neuber's rule, compute stress (KtS) at a notch with elastic assumptions and when the stress exceeds the strength of the material, the real stress will show somewhere on the materials stress-strain curve at a point σ.
  

• Several new boundary conditions are now supported under multi-loadcases including gravity, hydrostatic pressure, translational and rotational inertia, thermal loads, distributed mass and volumetric expansion/shrinkage.
  
• Result graph is supported.
  
• Export of deformed shape is supported.
  

• Orthotropic materials can be applied to plies within the laminates.
  
• Orthotropic material orientation can also be applied but it is limited to flat shapes. Separating/closing and Separating contact The contact conditions are now enhanced and made robust. The closing contact will work with gaps within the small-sliding zone. Any penetrations are automatically resolved when separating/ closing contact is used.
  

• Part info is available for several parts in the assembly.
  
• ECAD files reader has been updated.
  
• Spot weld visualization has been improved where 2T, 3T, and 4T spot welds can be visualized in different colors. The 2T spot welds are highlighted in red, 3T in cyan, and 4T in pink.
  
• The adaptation for sheets has been improved which should resolve several numerical instabilities that yield error ID 18.
  
• Data imported from CSV files can now read more decimal places.
  

• Issues with linear guide joint under virtual connectors.
  
• Laminate creation and editing have been re-factored to improve the workflow.
  
• Issues related to updating the units appropriately.
  
• Issues related to result Descriptions have been resolved.
  
• Issues with importing fatigue material properties from a CSV file to material database.
  
• Issues related to re-using adaptation from previous steps leading to performance issues.
  
• Remote loads are updated appropriately when edited.
  
• Improved display issues with selection of parts.
  
• Improved creation of connections.
  
• Improved creation of seam welds.
  
• Status bar is updated appropriately when solution is being prepared before solving.
  
• Improved approximation of spots, when thermal loads are applied on spots.
  
• Result quantity labels are fixed when running dynamic analysis with displacement base excitation.
  
• Fixed issues and inconsistencies related to creation of virtual connectors.
  
• Issues related to dynamic reactions along bushing coordinate system
  
• Improved error messages.
  
• Inconsistencies with Descriptionting and saving results.
  
• Fixed issues related to boundary condition visualization.
  
• Boundary conditions can be applied to the face where distribution mass is applied.
  
• Issues related to handling boundary conditions appropriately in local studies.
  
• Issues related to complex eigenvalue analysis linked to geometric nonlinear analysis.
  
• Issues related to selection of material database.
  
• Issues related to assembly info with laminates.
  
• Issues related to bookmarks.
  
• Issues related to bolt forces.
  
• Several crashes have been fixed.
  
• Several instabilities have been resolved with improved adaptation.
  

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