Numerical simulation of the FIRST (Fuel Injector Research for Sustainable Transport) configuration, experimentally investigated at DLR, with the ONERA CEDRE code. The numerical simulation is performed by coupling the CEDRE/CHARME fluid mechanics solver and CEDRE/SPARTE Lagrangian dispersed phase solver. The flame - identified on the left by an isosurface of heat release (orange) - is stabilized by an inner recirculation zone. Soot particles are produced in the lower part of the chamber and oxidized in the upper part, partly through secondary air injection - identified on the left by an isosurface of oxygen mass fraction (blue) - which reproduces the behavior of RQL (Rich burn, Quick-mix, Lean burn) aeronautical combustors. Experimental and numerical time-averaged fields of the soot volume fraction (in ppm) are compared on the right and show a good agreement.
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