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In this work the Sydney swirl stabilized burner for a hydrogen:methane fuel mixture is numerically modelledusing the OpenFOAM C++ library package. A non-reacting high swirl test case (N29S159) and a reactinglow swirl test case (SMH1) were investigated using Large Eddy Simulations and the Steady Laminar Flameletconcept. For the non-reacting case the velocity field components are in very good agreement with experimentalresults. For the reacting flow case the velocity components are also in excellent agreement with experimentalvalues, however the scalar quantities exhibit some under prediction. Possible reasons for the under predictionare discussed.

NON-PREMIXED SWIRL FLAME MODELLING USING THE OPEN SOURCE CFD PACKAGE OPENFOAM