Release 2025 R1 includes new features and enhancements for the following structural analysis disciplines:
Release 2025 R1 includes the following enhancements for analyses involving contact:
- 1.1.1. Enhanced Double-Sided Target Surfaces
- 1.1.2. Enhancements to Multipoint Constraints and Assemblies
- 1.1.3. Penalty And Augmented Lagrange Multiplier Introduced to Surface-based Constraint
- 1.1.4. Non-linear History File Now Includes Physical Time
- 1.1.5. Enhancements to Contact Data Tracking File
- 1.1.6. Contact Detection Improvements
Prior to this release, the double-sided target surface option (KEYOPT(8) = 1 of the TARGE170 element) is only valid only for the Gauss detection (KEYOPT(4) = 0 of the CONTA174 element) and "Normal from contact nodes" (KEYOTP(4) = 1,2 of CONTA174 element)). Now, the double-sided target surface option is also valid for "Projection-based method” (KEYOTP(4) = 3,4 of CONTA174 element and “Unified approach” (KEYOPT(4) = 5 of CONTA174).
Contact detection for the double-sided target surfaces is also refined to prevent missing constraint equations or bad crossing constraint equations for the MPC contact definition, greatly improving contact solution accuracy and robustness.
For more information, see see Double-Sided Target Surfaces in the Contact Technology Guide.
Selecting a constraint type for assemblies is problem-dependent and can have a significant impact on solution accuracy. In this release, the constraint type detection logic (KEYOPT(5) = 2 of target element) has been revised so that larger percentages of assembly models can be solved with improved robustness and accuracy, in particular for mixed constraint types (solid-to-solid, shell-solid, shell-to-shell) defined within a contact pair. For more information, see "TARGE170 Input Data" in the Element Reference.
To help resolve overconstraint conditions, penalty (KEYOPT(2) = 1) and augmented Lagrange multiplier (KEYOPT(2)=0) formulas are introduced to rigid and force-distributed types of surface-based constraint. They are suitable to relax constraint on surfaces nodes. These two formulae are also available to build spot weld connections using 3D node-to-surface contact element CONTACT175.
Physical time (for scaled wear analysis) is added into the non-linear history file, for fretting fatigue and bolt self-loosening problems where a map between simulation and physical time is needed. The total mechanical (EPTO) and total strain (EPTT) are also added in the solution tracking variable list.
The contact data tracking file (CND) format is changed for easy contact diagnosis. The convergence status and maximum penetration element (contact/target side) are added, and column values are rearranged with acronym on the top. The new CND format is easy to export into other plot forms.
Release 2025 R1 includes the following enhancements to elements and nonlinear technology used in structural analyses:
The INTER194, INTER195 3D gasket elements with thin solid option (KEYOPT(2) = 2) now support nonlinear material behavior based on ductile damage, in addition to von Mises plasticity.
Release 2025 R1 includes the following enhancements to material modeling and fracture analysis technology used in structural analyses:
Some material properties are not available via the material property menus of the GUI. For a list of such material properties, see GUI-Inaccessible Material Properties.
Material curve-fitting now supports shape memory alloy material models. Shape memory effect and super elasticity options are supported with uniaxial and biaxial test data.
ViscoElasticity fitting can involve multiple sets of experimental data at different temperatures for Shear and Modulus Bulk Decay. Partial solver options are now supported to address this situation with a multistep solution approach. The TBFT command can be issued to initiate the solves as needed (shear terms, bulk terms, and/or all experimental data). See Partial Solve Options Example for Prony Series Models for an example.
In material curve-fitting, AI-based automatic initialization (TBFT,AINI) of creep material parameters is now supported. For more information, see Creep Material Models and Initialize the Coefficients.
An example has been added to the Programmer's Reference to provide information on how to set up a UserMat API in C or C++.
You can now use the ductile damage model with INTER194 and INTER195 3D gasket elements with thin-solid option (KEYOPT(2) = 2: through-the-thickness, in-plane membrane, and transverse-shear deformation).
- Problems with Large Deflections
The fracture parameter J-integral calculation can now provide accurate results for both 2-D problems (PLANE182 and PLANE183) and 3-D problems (SOLID185 and SOLID186) with large deflections.
- Hyperelastic Materials
The fracture parameter J-integral calculation now supports isotropic hyperelastic materials with large deformation.
SMART crack-growth simulation now supports tabular loads, including those where ELEM and/or NODE are primary variables for temperature, displacement, and pressure loadings. You can now update the load tables after a load step or restart command, but you must use the initial mesh-based node and element numbering and not the current mesh after any changes (when ELEM and/or NODE are used as primary variables). For additional information and limitations, see SMART Crack-Growth Assumptions and Limitations in the Fracture Analysis Guide.
Release 2025 R1 includes the following enhancements for structural analyses involving linear dynamics:
Multithreading can be activated (using the -nt
command line
option) for HBM analysis to enable Shared-Memory Parallel (SMP) processing for
core harmonic computations. This option can significantly improve the
computation time for models with a higher number of linear degrees of freedom
and/or harmonics. For more details, see HBM Analysis and Parallel Processing in the Harmonic Balance Method Analysis Guide.
Linear perturbation analysis is now supported for a component mode synthesis
generation pass where the element results calculation is activated
(Elcalc
= YES on the CMSOPT
command).