HyperWorksEngineering Solutions is a modeling and visualization environment for NVH, Crash, CFD, Drop Test and Aerospace using best-in-class solver
technology.
The Crash application offers a tailored environment in HyperWorks that efficiently steers the Crash CAE specialist in CAE model building, starting from CAD geometry and finishing with
a runnable solver deck in Radioss, LS-DYNA and PAM-CRASH 2G.
HyperWorks offers high quality tools for CFD applications enabling the engineer to perform modeling, optimization and post-processing
tasks efficiently.
The Drop Test Manager is an automated solution that allows you to either simulate a single drop test or a choice of
multiple iterations with the aim of finding the sensitivity of process variables like initial orientation and drop
height in a typical drop test by controlling the run parameters and conditions with ease.
Many essential utility tools using HyperWorks-Tcl have been developed over the years to support Aerospace customers. A few tools have been collected and upgraded to
be compatible with this release.
Browsers supply a great deal of view-related functionality in Engineering Solutions by listing the parts of a model in a tabular and/or tree-based format, and providing controls inside the table
that allow you to alter the display of model parts.
Smooth Particle Hydrodynamics (SPH), Finite Point Method (FPM) is a technique used to analyze bodies that do not have
high cohesive forces among themselves and undergo large deformation, such as liquids and gases.
1D mesh that allows accurate testing of connectors, such as bolts, and similar rod-like or bar-like objects that can
be modeled as a simple line for FEA purposes.
Automatically generate a mesh at the midplane location, directly from the input geometry (components, elements, solids
or surfaces), without first creating a midsurface.
Shrink wrap meshing is a method to create a simplified mesh of a complex model when high-precision models are not
necessary, as is the case for powertrain components during crash analysis.
Loose wrap wraps the selected elements or components, surfaces, or solids with the target element size specified,
and outputs an outer-volume mesh which approximately adheres to the original FE topology.
Tight wrap creates a wrapped surface mesh which adheres as closely as possible to the original FE topology representation,
automatically detecting and following the surface features of the model.
2D BL meshing is a method to create a 2D mesh with or without boundary layers on planar sections defined by sets/groups
of edges defining closed loops.
Volume mesh or "solid meshing" uses three-dimensional elements to represent fully 3D objects, such as solid parts
or sheets of material that have enough thickness and surface variety that solid meshing makes more sense than 2D shell
meshing.
Perform automatic checks on CAD models, and identify potential issues with geometry that may slow down the meshing
process using the Verification and Comparison tools.
Shrink wrap meshing is a method to create a simplified mesh of a complex model when high-precision models are not
necessary, as is the case for powertrain components during crash analysis.
Tight wrap creates a wrapped surface mesh which adheres as closely as possible to the original FE topology representation,
automatically detecting and following the surface features of the model.
Tight wrap creates a wrapped surface mesh which adheres as closely as possible to the
original FE topology representation, automatically detecting and following the surface
features of the model.
The accuracy of the output is dictated by the element size: the larger the element
size the less detail, the smaller the element size the more detail. This algorithm
works differently than the loose wrap in that it projects the nodes of the shrink
wrap to the original mesh, hence it is able to more accurately capture features.
Comparison of Tight and Loose Meshing
Notice the differences between tight and loose meshing, especially in the pulleys on
the front of the engine and the resulting width of the individual cylinder exhaust
pipes.
Comparison of Altering the Jacobian Value for Solid Mesh Generation
Within both tight and loose wrap algorithms there is an option to generate solid
mesh. This will generate an all-hexa mesh on completion of the shrink wrap. When the
generate solid mesh checkbox is active it exposes a
minimum jacobian input; this option essentially hexa meshes the part with this
element quality criteria defined. It controls the hexa quality which is directly
linked to the adherence to the topological features of the original component. The
jacobian value must be between 0 and 1. The nearer the value is to 1 the cruder the
output will appear (the mesh will be more heavily voxelised). When the value is
closer to 0, you allow the shrink wrap solid mesh algorithm to smooth and adhere to
more features while maintaining the solid mesh minimum jacobian element quality. By
default the minimum jacobian value is 0.3.
Shrink Wrapping with Feature Recognition
An additional option can be used to manually define features which will be adhered to
during the meshing process. Typically, when using the shrink wrap the mesh attempts
to follow features, but has some freedom to break away from original edges of the
part. However, when the features are manually selected within the panel the
resultant shrink wrap mesh will follow the chosen features. This can be important
when defining a face of a component that may be in contact with other parts, or
there may just be a feature that needs to be recognized and adhered to and cannot be
approximated for whatever reason.
Comparison of using Global and Local Systems for Mesh Orientation
There is also an advanced option to control the mesh orientation. If you have a
non-uniform part and you want to re-orientate the mesh so that it follows the
features of the original component better then you can use this option. By default
the mesh orientation always adheres to the global system, however, you can generate
a local coordinate system and override the default behavior.
In the example below, you can see the original mesh, the default shrink wrap mesh
using the global system, and the new re-orientated mesh using the local coordinate
system.