Combustion chambers are naturally prone to acoustic instabilities that originate from flame propagation. Passive devices such as combustor chamber baffles, resonators, and injection liners have proven to attenuate acoustic instabilities degradate the integrity of engine components. Acoustic energy viscous dissipation effects are measured and quantified for new designs and arrangements implemented in tested suppression devices. Two passive suppression devices are introduced which exhibit new baffle arrangement and combustion liner design. Audio acoustic equipment excites chamber acoustic instabilities and microphones receive acoustic pressure wave amplitudes. Using this technique viscous damping effects from acoustic sound waves are measured...
Combustion instability in jet engines impedes efficient burning of fuel and degrades engine performa...
A damping device combining low flow resistance with high acoustic damping has be en developed. Such ...
Combustion instabilities in rocket engines are caused by coupling between the combustion processes a...
Combustion chambers are naturally prone to acoustic instabilities that originate from flame propagat...
International audienceWhen coupled to acoustics, unsteady heat release oscillations may cause recurr...
One of the major technical issues in the development of liquid propellant rocket engines is the high...
Combustion instability is recognized as one of the major problems frequently faced by engineers duri...
Combustion instabilities can be self-excited through a feedback loop between unsteady heat release a...
Thermo-acoustic instability results in large amplitude oscillations in pressure and heat release. Th...
On secondment from Rolls-Royce plc Thermo-acoustic instabilities in lean gas turbine combustors have...
International audienceDespite extensive efforts, controlling combustion instabilities in modern gas ...
Combustion instabilities are caused by a coupling between acoustic waves and unsteady heat release. ...
Results of a computational study on the effectiveness of various passive devices for the control of ...
The excitation of acoustic oscillations in combustion chambers is well-known as an unwelcome phenome...
International audiencePassive control of combustion instabilities is explored in the case of systems...
Combustion instability in jet engines impedes efficient burning of fuel and degrades engine performa...
A damping device combining low flow resistance with high acoustic damping has be en developed. Such ...
Combustion instabilities in rocket engines are caused by coupling between the combustion processes a...
Combustion chambers are naturally prone to acoustic instabilities that originate from flame propagat...
International audienceWhen coupled to acoustics, unsteady heat release oscillations may cause recurr...
One of the major technical issues in the development of liquid propellant rocket engines is the high...
Combustion instability is recognized as one of the major problems frequently faced by engineers duri...
Combustion instabilities can be self-excited through a feedback loop between unsteady heat release a...
Thermo-acoustic instability results in large amplitude oscillations in pressure and heat release. Th...
On secondment from Rolls-Royce plc Thermo-acoustic instabilities in lean gas turbine combustors have...
International audienceDespite extensive efforts, controlling combustion instabilities in modern gas ...
Combustion instabilities are caused by a coupling between acoustic waves and unsteady heat release. ...
Results of a computational study on the effectiveness of various passive devices for the control of ...
The excitation of acoustic oscillations in combustion chambers is well-known as an unwelcome phenome...
International audiencePassive control of combustion instabilities is explored in the case of systems...
Combustion instability in jet engines impedes efficient burning of fuel and degrades engine performa...
A damping device combining low flow resistance with high acoustic damping has be en developed. Such ...
Combustion instabilities in rocket engines are caused by coupling between the combustion processes a...