Computational Grids
Complex Geometries and Fields
CAD Creation - Parametric Design

Wing-Body-Pylon-Nacelle Configuration

This geometry represents airflow over a transonic transport aircraft, complete with a pylon and flow-through nacelle attached to the wing. A hybrid mesh was generated using CENTAUR containing both prisms in the boundary layer and tetrahedra in the interior. A symmetry plane was used so that only half the geometry needed to be modeled.