Indirect combustion noise, generated by the acceleration and distortion of entropy waves
through the turbine stages, has been shown to be the dominant noise source of gas turbines …

Combustion noise has recently been the subject of attention of both the aeroacoustic and
the combustion research communities. Over the last decades, engine manufacturershave …

Nowadays, engines powering modern and large commercial or military aircraft essentially
rely on gas turbine technologies. Since the first prototypes built in the 40's, the efficiency and …

In modern ultra-high by-pass ratio turboengines, the noise contribution of both turbine
stages and combustion chamber is expected to increase drastically. In the present work …

The contribution of combustion noise to the total acoustic emissions of the aircraft has
increased in commercial airplanes as the noise generated by other sources such as jet and …

Generation of combustion noise is here studied in a realistic turbine stage configuration,
where the temperature fluctuations generated by an aeronautical burner (responsible of the …

Indirect combustion noise, generated by the acceleration and distortion of entropy waves
through the turbine stages, has been shown to be the dominant noise source of gas turbines …

Air transportation is an essential part of modern business and leisure needs, and the
number of passengers carried per year is rapidly increasing worldwide. The International …

Combustion noise is increasing its relative contribution to aircraft noise, while other sources
are being reduced and new low-NOx emission combustion chambers being built. Two …

Afin d'augmenter le rendement et la puissance spécifique des turbines à gaz, la température
en entrée de la turbine haute pression a été continuellement augmentée, au point …