Abstract: The aim of the present work is to evaluate the ability of large eddy simulation (LES) to predict flame shape and structures in a two-stage two-injection burner representative of new generation staged aeronautical engine: ...

Abstract: The BIMER combustor is a lab-scale burner investigating fuel staging techniques as a stabilization strategy for lean premixed prevaporized combustion for aeronautical applications. Two stages compose its injection system: ...

Abstract: This paper presents an experimental study of lean flames stabilization with nanosecond repetitively pulsed discharges. The two-stage, swirled-stabilized, multipoint injector BIMER operates at atmospheric pressure with ...