Engineering Solutions is a modeling and visualization environment for NVH, Squeak and Rattle Director, Crash, CFD, 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.
It is convenient to apply aerospace loads and concentrated mass that is predefined at specific node ID’s from an Excel
file. This requires carefully numbering nodes with specific ID’s, which is a standard practice in aerospace.
Line loads allow total loads (forces and moments) to be applied in a distributed manner on nodes even though the load
is applied on geometry lines or set of nodes forming ordered edges.
Aircraft windows are normally modeled with CROD elements around the hole of the shells. Constant pressure on the window
area is applied by means of force distribution on the edge nodes.
Use the Transformation Tool to translate, scale, reflect or rotate elements with multiple numbers of copies, including
properties and loads, attached to them.
Use multiple combinations of source files (in the form of CSV) and multiple target models (decks or HyperMesh .dbs) to realize field mapping for the creation of new loads, such as temperature and pressure.
Use the Plot SPC/SPCD tool to display the SPC/SPCD assigned to the nodes in their relevant analysis (output) system.
The tool shows the coefficients of the selected degrees of freedom (DOF) and the ID of the system associated to the
node(s) where the constraint is applied.
Browsers supply a great deal of view-related functionality 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.
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.
PLOAD1 Create and Review
Create and review pressure loads on 1D elements that are fully or partially loaded.
Map Force, Mass, Temperature
It is convenient to apply aerospace loads and concentrated mass that is predefined at specific node ID’s from an Excel file. This requires carefully numbering nodes with specific ID’s, which is a standard practice in aerospace.
Line Loads
Line loads allow total loads (forces and moments) to be applied in a distributed manner on nodes even though the load is applied on geometry lines or set of nodes forming ordered edges.
Window Pressure
Aircraft windows are normally modeled with CROD elements around the hole of the shells. Constant pressure on the window area is applied by means of force distribution on the edge nodes.
Transform Elements
Use the Transformation Tool to translate, scale, reflect or rotate elements with multiple numbers of copies, including properties and loads, attached to them.
Field Looper
Use multiple combinations of source files (in the form of CSV) and multiple target models (decks or HyperMesh .dbs) to realize field mapping for the creation of new loads, such as temperature and pressure.
Plot SPC/SPCD
Use the Plot SPC/SPCD tool to display the SPC/SPCD assigned to the nodes in their relevant analysis (output) system. The tool shows the coefficients of the selected degrees of freedom (DOF) and the ID of the system associated to the node(s) where the constraint is applied.