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PDOC-DMPE-2023-02

DMPE
Palaiseau
À Pourvoir
Mots-clés: 
Combustion, flame structure, high-speed optical diagnostics
Intitulé: 
Experimental study of the influence of the insertion geometry of an injector on the extinction limit of an aeronautical combustion chamber under representative engine conditions
Contact: 
guillaume.pilla@onera.fr