This case study on combustion and radiative heat transfer in a generic gas turbine (GGT) combustor of TU Darmstadt illustrates the multi-physics modeling capabilities in OMNIS™/Open-DBS.

Recent developments in NUMECA OMNIS™/Open-DBS have yielded impressive improvements in massively parallel performance. 

Meshing is always a compromise between computational efficiency and the needed accuracy. We need the smallest possible mesh to capture the effects that we consider as the most important inf our simulations.

The goal of turbomachinery CFD simulations is to predict flow behavior in adjacent rotating and non-rotating blade rows. The link between these rotating and stationary frames of reference is called the Rotor-Stator interface.