The use of fossil fuel is expected to increase significantly by midcentury because of the large
rise in the world energy demand despite the effective integration of renewable energies in …

This review overviews combustion technologies for reduced emissions and better fuel
economy in the industrial gas turbine. Lean premixed combustion (LPM) technology is …

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 …

Gas turbine engines are prone to the phenomenon of thermoacoustic instability, which is
highly detrimental to their components. Recently, in turbulent combustors, it was observed …

In a can-annular gas turbine combustion system, low-frequency self-excited combustion
instabilities can arise from coupled interactions between adjacent can combustors, rather …

An investigation of self-excited combustion instabilities in a RP-3 fueled, multi-swirl
stabilized, lean direct injection (LDI) combustor was performed and investigated with …

Multi-element injector configurations, typically comprising numerous small-scale jet nozzles,
will be required to enable reliable lean-premixed gas turbine combustion operating with …

Self-excited combustion instabilities in a mesoscale multinozzle array, also referred to as a
micromixer-type injector, have been experimentally investigated in a lean-premixed tunable …

This paper shows the importance of considering the thermal state of a combustor to
investigate or predict its thermoacoustic stability. This aspect is often neglected or regarded …

Understanding the response of multi-jet turbulent hydrogen-air flames to acoustic forcing is
key for the development of future carbon-neutral gas turbine combustors. In this paper, we …