Menu principal
Vous êtes ici
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
S'abonner aux offres
