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Simultaneous measurements of Planar Laser-Induced Fluorescence (PLIF) kerosene and PLIF-OH have been successfully performed in a multipoint injection system for various overall equivalence ratios, air inlet temperatures between 480 and 730 K, and pressures up to 2.2 MPa. Single-shot two-dimensional (2D) maps of the spatial distribution of kerosene vapor and OH radical in the combustor have been recorded with good signal-to-noise ratio. Results show that depending on the split between the pilot and the main injectors, the §ame front exhibits either a single or a double structure. Good spatial correlation between the repartition of kerosene vapor and the position of the §ame front was

Investigation of performances of innovative aeronautic injection systems using advanced laser diagnostics