Tips & Tricks

Horse saddle distortion modelling in Visual Weld
Welding of structures involves complex interactions between thermal, metallurgical and mechanical phenomena leading to residual stresses and distortions, which play a major role during subsequent service of these structures. Controlling material characteristics, residual stress and keep distortion within tolerances via the computer can significantly enhance the performance, the quality of the product and the structure’s service life
Mandikizinoyou Taro Sheet Metal Forming, Virtual Manufacturing, Multiphysics, Welding & Assembly

Overview of CSM Welding Advisor in Visual Environment 18.0.2
This tip is to give an overview of new CSM welding advisor in Visual Environment 18.0.2. This new advisor comes in replacement of Visual Welding advisor and uses Assembly solver to perform transient welding simulation.
Mandikizinoyou Taro Sheet Metal Forming, Virtual Manufacturing, Welding & Assembly

Demonstrator of typical Stamp-Assembly process in automotive BiW manufacturing
New Stamp-Assembly non-confidential tutorial available
Jan Bejvl Sheet Metal Forming, Welding & Assembly, Virtual Integration Platform

Using Region sources in CFD-VisCART
In order to control grid spacing at user-defined locations, mesh sources are a common tool in CFD-VisCART (Figure 1). Point, Line, Curve, Plane, Box and Surface sources have been available for several years. Cylinder and Sphere sources were introduced a few years back. To extend this tool set further, CFD-VisCART V2013.0 introduced Region sources.
Abraham Meganathan CFD

Automatic covering of larger unwanted holes in CFD-VisCART
CFD-VisCART meshing automatically closes or covers holes in the geometry that are smaller in size than the cell size specified at the surfaces. To cover LARGER holes, the ‘Max Hole Size to Cover’ feature can be used. This feature, introduced in V2013.2, works to automatically cover larger holes in the geometry during mesh generation, and thus prevents the mesh from leaking into unwanted regions. This feature is available with all mesh types supported in CFD-VisCART.
Abraham Meganathan CFD

Internal injection lines modeling
Internal injection lines on a shell model (i.e. made of internal element edges) are not supported by the parallel solver.
Mathilde Chabin Composites

Direct Opening of a mesh
The creation of a RTM project and loading of the model mesh is usually done in 2 steps.
Mathilde Chabin Composites

Coupling between PAM-FORM and PAM-RTM: multiple part mapping
Coupling between PAM-FORM 2G and PAM-RTM is done through a .DSY file. Thus, pre-forming process is simulated with PAM-FORM 2G and resulting fiber orientations that will affect permeabilities are transferred to PAM-RTM model setup.
Mathilde Chabin Composites

Grouping parts during data import in CFD-VisCART
When dealing with complex industrial models such as cars and airplanes, hundreds of parts need to be managed. Each one of these parts may also be subdivided into different components. In order to easily manipulate these different parts and components in CFD-VisCART, you can make use of the grouping feature.
Abraham Meganathan CFD

CFD-VisCART: Mesh Extrusion
In most CFD simulations, it is required to place inlets/outlets far enough from the region of interest in order to reduce their influence on the solution. In many applications, this can be done by extruding existing inlets/outlets BC patches away from the domain.
Abraham Meganathan CFD