Flame propagation in aeronautical swirled multi-burners: Experimental and numerical investigation - Archive ouverte HAL
Article Dans Une Revue Combustion and Flame Année : 2014

Flame propagation in aeronautical swirled multi-burners: Experimental and numerical investigation

Résumé

Driven by pollutant emissions stringent regulations, engines manufacturers tend to reduce the number of injectors and rely on lean combustion which impacts the light-around phase of ignition. To improve knowledge of the ignition process occurring in real engines, current research combines fundamental and increasingly complex experiments with high fidelity numerical simulations. This work investigates the flame propagation, using a multi-injector experiment located at CORIA (France) in combination with Large Eddy Simulation (LES) obtained by CERFACS (France). The comparison of numerical fully transient ignition sequences with experimental data shows that LES recovers features found in the experiment. Global events such as the propagation of the flame front to neighboring swirlers are well captured by LES, with the correct propagation mode (spanwise or axial) and the correct overall ignition time delay. The detailed analysis of LES data allows to identify the driving mechanisms leading to each propagation mode. (C) 2014 The Combustion Institute. Published by Elsevier Inc. All rights reserved.
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Dates et versions

hal-01612415 , version 1 (06-10-2017)

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David Barre, Lucas Esclapez, Matthieu Cordier, Eleonore Riber, Bénédicte Cuenot, et al.. Flame propagation in aeronautical swirled multi-burners: Experimental and numerical investigation. Combustion and Flame, 2014, 161 (9), pp.2387--2405. ⟨10.1016/j.combustflame.2014.02.006⟩. ⟨hal-01612415⟩
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