The following model shows how an axial gas turbine geometry, including all the secondary hub and shroud flow paths and the internal cooling geometry, is prepared for analysis.

This tutorial will show the entire process flow of a typical BOXERmesh project for creating a solvable, refined mesh on a quasi-2D aerofoil section. This includes specifying a bounding box and region, setting edge and face refinement levels, patch creation and defining a viscous layer mesh. After the mesh sizing and refinement parameters are specified, the mesh is created, visualised and saved to file.

In this case we want to produce meshes for the metal and fluid phases for two connected pieces of pipe, with a continuous fluid domain running through them. The metal phase of each pipe will have a separate mesh domain, connected by a conformal interface; the two pipes may be made of different materials, or there is a gasket between the abutting faces which we do not want to model directly, so we wish to mesh more than one region.

Shows how to use sketching primitives to repair and augment an existing geometry. The primitive sketching entities are then converted to ‘real’ geometry and a mesh is created.

This tutorial looks at how to actuate a mannequin by moving the arms, legs and trunk. We will also use the parametric function to collect all of the separate transformations under a single, controllable parameter.