Some aspects of turbulence and combustion modeling of swirl-stabilized LPP combustion

摘要

Results of application of the maximum flowrate principle to correct the k- epsilon turbulence model in swriling flow situations are presented. Non-reacting swriling flows with and without heat transport as well as reacting swirl flows are analyzed. Combustion of A-jet fuel in stoichiometric and lean regimes is simulated. A realistic 3-d swirl-combustor geometry is used in computations.