ANSYS, Inc. Release Notes
This section contains information about Release 14.0 enhancements not listed elsewhere in this document.
ANSYS, Inc. continues to refine the Mechanical APDL documentation set. To that end, the following changes and enhancements to the documentation have occurred with this release:
The following new example problems have been added to the Technology Demonstration Guide:
This example problem demonstrates how to model a fluid that is fully enclosed by a solid (the container). The problem shows how loading on the container and container deformation affect the pressure, volume, density and mass of the contained fluid. Highlights include modeling hydrostatic fluid elements with negative and positive volumes, use of a gas material model, and reinforcing.
This example problem demonstrates how to simulate stent-artery interaction during and after stent placement in an occluded artery. The analysis uses advanced modeling techniques including contact, element birth and death, mixed u-P formulation, and nonlinear stabilization.
This example problem demonstrates the capabilities and advantages of the surface-projection-based contact method in a highly nonlinear problem. This analysis of a rubber boot seal model includes geometric, material, and changing status nonlinearities (contact). Highlighted analysis capabilities include 3-D surface-to-surface contact element technology, surface-projection-based contact, and the use of Neo-Hookean hyperelastic material.
This example problem is the second of two problems that simulate a rocket nozzle. The new problem demonstrates how to simulate the thermal stresses induced during the operation of the nozzle. (The existing problem demonstrates how to simulate the thermal stresses during the manufacturing stage of a rocket nozzle.)
It is assumed that the rocket has been launched and that hot gases are flowing through the nozzle, subjecting the inside and outside of the nozzle body to convection heat loading. The heat loading leads to a significant thermal gradient through the thickness of the body that manifests as high thermal stresses. Solid thermal and structural elements accurately simulate the multiphysics of the problem. While a fully coupled element could solve the problem, a loose coupling method is used instead. Because the body material could be homogenous or a layered composite, the simulation requires a solid element type with both homogeneous and layered material capabilities.
Hot-rolling is a metal-forming process occurring above the recrystallization temperature of the material. Many types of hot-rolling processes exist, including structural shape rolling, where a component is passed through rollers to achieve the desired shape and cross section. Structural steel is the most common hot-rolled material.
In this example problem, the hot-rolling process to form the I-beam is simulated statically using rezoning to repair a severely distorted mesh in a 3-D large-deformation analysis. The analysis also uses contact technology and symmetric expansion.
This example problem demonstrates how to simulate the friction stir welding (FSW) process. Several typical characteristics of FSW are presented, including plastic deformation, tool-workpiece surface interaction, and heat generation due to friction and plastic deformation. Thermal and mechanical behaviors are mutually dependent and coupled together during the process. A nonlinear direct coupled-field analysis is performed. Highlighted analysis capabilities include direct structural-thermal analysis using solid coupled-field elements, frictional heat generation using contact elements, plastic heat generation in coupled-field elements, and use of surface-projection-based contact.
This example problem demonstrates the use of acoustic elements coupled with structural elements to analyze the performance of a speaker assembly. Highlights include structural-acoustic coupling using fluid-structure interaction (FSI) in 3-D, a symmetric FSI algorithm, perfectly matched layers (PML) to absorb outgoing acoustic waves, sound pressure level (SPL) and velocity postprocessing, far-field postprocessing of acoustic field, and user-defined symmetric expansion options.
Additional legacy features, commands, elements, and theory information have been moved to the Feature Archive. While ANSYS, Inc. continues to support these legacy capabilities for the immediate future, some may be undocumented in future releases. You are urged to consider moving to their recommended replacements.
Release 14.0 offers the new Material Reference. The reference provides a single, convenient resource for information about the available material models, linear and nonlinear material properties, material data tables, material model combinations, explicit dynamics materials, element support for material models, and other important information. Expect to see ongoing improvements in subsequent releases.
Release 14.0 offers an improved Element Reference. The reference provides a single, convenient resource for information about element classifications, types, and features. Expect to see ongoing improvements in subsequent releases. To get started immediately, see Selecting Elements for Your Analysis.
All topics related to parallel processing have been moved into the new Parallel Processing Guide. The guide includes the following primary topics: shared memory parallel, distributed memory parallel (Distributed ANSYS), and GPU acceleration. All of these topics had been previously located in various other guides.
The following documentation updates are available for programmers:
Routines and functions documented in the Programmer's Manual have been updated to reflect the current source code. To see specific changes in a file, ANSYS, Inc. recommends opening both the old and current files (using a text editor that displays line numbers), then comparing the two to determine which lines have changed. You can copy the updated files to your system by performing a custom installation of the product.
Memory and CPU time have been significantly reduced when large element and/or node IDs are used, especially when large gaps exist in the element or node numbering.
Many more compute-intensive operations, including graphics, are now using shared-memory parallel if activated.
The following enhancements have been made to the POST1 general database results postprocessor.
LCOPER with Oper2 = CPXMAX now calculates the equivalent strain.
The time at which fatigue stresses occurred (from the SET command or manually input via the FS command) is now captured. Time is not used in the fatigue calculation and is only for reference purposes.
LaRc03/04 failure criteria are now available for failure analysis with both plain stress and full 3-D stress states. The two new failure criteria sets are based on various composite fiber and matrix failure mechanisms and account specifically for failure due to fiber kinking. While LaRc03/04 failure criteria can apply to general orthotropic materials, they are most suitable for unidirectional fiber-reinforced composites.
If you wish to control the maximum amount of memory that the program uses, you can do so by specifying a negative value for -m on the command line, or by specifying a negative value for the Total Workspace in the Command Launcher. By default, the program continues to dynamically grow memory as needed; however, specifying the negative value allows you to stop this dynamic growth. If the program requires additional memory beyond what is available, however, it will fail to proceed rather than use disk space as virtual memory.
The database (-db) memory space may grow dynamically as well if system resources (RAM and paging space) are sufficient. To use a fixed space instead, specify a negative value for -db on the command line, or specify a negative value for the database in the Command Launcher. If you use a fixed space and the database requires more space, the program writes to Jobname.page as in prior releases.
APDL Math extends the APDL scripting environment of Mechanical APDL to give you access to the powerful matrix manipulation routines in the Mechanical APDL product. A number of new functionalities have been added to the APDL Math feature in this release. These enhancements give you the ability to:
Perform a dot (or inner) product of two vectors (new *DOT command).
Perform a Fast Fourier transformation of a specified matrix or vector (new *FFT command).
Initialize a vector or dense matrix (new *INIT command).
Link to an existing matrix, thus providing a means to manipulate a submatrix of the original matrix (*DMAT command).
Export a matrix in the DMIG file format (*EXPORT command).
Normalize a vector (*NRM command).
Resize an existing matrix or vector (*DMAT and *VEC commands).
Compute absolute values of complex numbers via the new CXABS parametric function.
Access real and imaginary parts of complex numbers.
List all APDL Math objects (*STATUS,MATH command).
For more information, see "APDL Math" in the ANSYS Parametric Design Language Guide.
The default file split size (/CONFIG,FSPLT) of 2000 GB (2 TB) has been removed. Files will no longer split by default.