Combustion noise in gas turbine engines has recently become a relevant source of noise in
the aircraft due to the appearance of new burner architectures that are intrinsically more …

Ignition in annular multi-burner combustors is marked by a succession of four phases,
ending with a characteristic flame expansion from burner to burner, often referred to as light …

SAFRAN Helicopter Engines has developed the spinning combustion technology in which
the burnt gases from one injector travel tangentially along the combustor annulus towards …

During the ignition of a swirled single-injector combustor, two phases have been identified
experimentally. In the first, the flame penetrates the injection unit, while in the second, the …

SAFRAN Helicopter Engines has recently developed the spinning combustion technology in
which the burnt gases from one injector travel tangentially along the combustor annulus …

Thermoacoustic combustion instabilities continue to be a major hurdle in the development of
future gas turbine combustion systems. These instabilities are char-acterized by large …

Abstract Combustion in Liquid Rocket Engines (LRE) happens in extreme conditions which
imply several multi-physics phenomena. For this reason, numerical simulation is used to …