A review of aircraft subsonic and supersonic combustors
Combustion is an essential process for generating propulsion for most existing aircraft. The
combustion processes, such as ignition, flame propagation, and flame stability, are …
combustion processes, such as ignition, flame propagation, and flame stability, are …
[HTML][HTML] The effect of hydrogen enrichment, flame-flame interaction, confinement, and asymmetry on the acoustic response of a model can combustor
E Æsøy, T Indlekofer, F Gant, A Cuquel… - Combustion and …, 2022 - Elsevier
To maximise power density practical gas turbine combustion systems have several injectors
which can lead to complex interactions between flames. However, our knowledge about the …
which can lead to complex interactions between flames. However, our knowledge about the …
Combustion dynamics of multi-element lean-premixed hydrogen-air flame ensemble
The crux of the technical issues facing the development of hydrogen gas turbine engines is
the problem of how to enable low NOx, low dynamics combustor operations without …
the problem of how to enable low NOx, low dynamics combustor operations without …
Experimental investigation of combustion dynamics and NOx/CO emissions from densely distributed lean-premixed multinozzle CH4/C3H8/H2/air flames
Lean-premixed fuel-flexible combustion technology capable of operating on a wide range of
fuels, including high or pure hydrogen, is expected to play a crucial role in reducing nitrogen …
fuels, including high or pure hydrogen, is expected to play a crucial role in reducing nitrogen …
System identification and early warning detection of thermoacoustic oscillations in a turbulent combustor using its noise-induced dynamics
Despite significant research, self-excited thermoacoustic oscillations continue to hinder the
development of lean-premixed gas turbines, making the early detection of such oscillations …
development of lean-premixed gas turbines, making the early detection of such oscillations …
Mutual synchronization of two lean-premixed gas turbine combustors: Phase locking and amplitude death
In a can-annular gas turbine combustion system, low-frequency self-excited combustion
instabilities can arise from coupled interactions between adjacent can combustors, rather …
instabilities can arise from coupled interactions between adjacent can combustors, rather …
Cross-talk-interaction-induced combustion instabilities in a can-annular lean-premixed combustor configuration
The prediction of self-excited combustion instabilities in a can-annular gas turbine
combustion system is a significant challenge, mainly because the instabilities originate from …
combustion system is a significant challenge, mainly because the instabilities originate from …
Influence of the co-and counter-swirl on combustion instability of the centrally staged combustor
The centrally staged combustor is an effective way to reduce NOx emissions from
combustors. However, combustion instability caused by the mutual coupling between flames …
combustors. However, combustion instability caused by the mutual coupling between flames …
Experimental investigation of combustion instability in a centrally staged combustor under self-excited oscillation conditions
This paper presents an experimental investigation of combustion instability and flame
dynamics in a laboratory-scale lean premixed prevaporized centrally staged combustor …
dynamics in a laboratory-scale lean premixed prevaporized centrally staged combustor …
Experimental study on flame/flow dynamics in a multi-nozzle gas turbine model combustor under thermo-acoustically unstable condition with different swirler …
This paper presents an experimental study on the combustion stability characteristics and
flame/flow dynamics in a multi-nozzle, lean premixed prevaporized (LPP), swirl-stabilized …
flame/flow dynamics in a multi-nozzle, lean premixed prevaporized (LPP), swirl-stabilized …