Engineering Solutions is a modeling and visualization environment for NVH, Squeak and Rattle Director, Crash, CFD, and Aerospace using
best-in-class solver technology.
In this tutorial, you will learn to generate boundary layer type meshes with an arbitrary number of layers and thickness
distribution, which can be used for CFD applications, molding simulations, or other processes. You will also generate
automatically a distributed thickness distribution to prevent boundary layer interference /collision in zones
where the distance between opposing walls is too small to accommodate the baseline or nominal boundary layer thickness.
In this tutorial, you will learn to generate meshes for CFD applications, for example Fluent and STAR CD using the CFD Tetramesh panel, generate boundary layer type meshes with an arbitrary number of layers and
thickness distribution, specify/identify boundary regions for CFD simulations, export a mesh with boundary regions
for Fluent, and import the model into Fluent.
In this tutorial, you will learn to generate meshes for most CFD codes using the CFD Tetramesh panel and generate
boundary layer type meshes with arbitrary number of layers and thickness distribution in domains defined by surfaces
that are very close to one another in some areas. More specifically, in some areas the clearance or separation of
bounding surfaces is not enough to accommodate the user specified nominal boundary layer thickness. You will
also learn to generate a distributed thickness “loading” that prevents boundary layer interference/collision in zones
where the distance between opposing walls is too small to accommodate the baseline or nominal boundary layer thickness.
In this tutorial, you will learn to generate 2D boundary layer type meshes with an arbitrary number of layers and
thickness distribution in domains defined by edges. You will also generate 2D boundary layer type meshes in areas
where the clearance or separation of bounding edges is not enough to accommodate the user specified nominal boundary
layer thickness/number or layers.
In this tutorial you will learn how to generate a structured quad surface mesh, adjust the boundary layer thickness
manually and generate a hybrid grid (tetramesh with boundary layer). You will also export the model for a CFD solver
of your choice.
This exercise will cover how to take results from a CFD analysis and apply them to a new model for heat transfer or
structural analysis. Using the linear interpolation tools within Engineering Solutions, results from a CFD analysis
can be transferred to be loads in an analysis to be run in OptiStruct or any other supported solver.
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.
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.
CFD-1100: Create a Hybrid Grid with Varying Boundary Layer Thickness
In this tutorial, you will learn to generate boundary layer type meshes with an arbitrary number of layers and thickness distribution, which can be used for CFD applications, molding simulations, or other processes. You will also generate automatically a distributed thickness distribution to prevent boundary layer interference /collision in zones where the distance between opposing walls is too small to accommodate the baseline or nominal boundary layer thickness.
CFD-1000: Create a Hybrid Grid Using the CFD Mesh Panel
In this tutorial, you will learn to generate meshes for CFD applications, for example Fluent and STAR CD using the CFD Tetramesh panel, generate boundary layer type meshes with an arbitrary number of layers and thickness distribution, specify/identify boundary regions for CFD simulations, export a mesh with boundary regions for Fluent, and import the model into Fluent.
CFD-1200: CFD Meshing with Automatic BL Thickness Reduction
In this tutorial, you will learn to generate meshes for most CFD codes using the CFD Tetramesh panel and generate boundary layer type meshes with arbitrary number of layers and thickness distribution in domains defined by surfaces that are very close to one another in some areas. More specifically, in some areas the clearance or separation of bounding surfaces is not enough to accommodate the user specified nominal boundary layer thickness. You will also learn to generate a distributed thickness “loading” that prevents boundary layer interference/collision in zones where the distance between opposing walls is too small to accommodate the baseline or nominal boundary layer thickness.
CFD-1300: Plane 2D Meshing with Boundary Layers
In this tutorial, you will learn to generate 2D boundary layer type meshes with an arbitrary number of layers and thickness distribution in domains defined by edges. You will also generate 2D boundary layer type meshes in areas where the clearance or separation of bounding edges is not enough to accommodate the user specified nominal boundary layer thickness/number or layers.
CFD-1500: Use Distributed Thickness for Varying Boundary Layer Thickness
In this tutorial you will learn how to generate a structured quad surface mesh, adjust the boundary layer thickness manually and generate a hybrid grid (tetramesh with boundary layer). You will also export the model for a CFD solver of your choice.
CFD-1600: Map CFD Results
This exercise will cover how to take results from a CFD analysis and apply them to a new model for heat transfer or structural analysis. Using the linear interpolation tools within Engineering Solutions, results from a CFD analysis can be transferred to be loads in an analysis to be run in OptiStruct or any other supported solver.