Turbulent combustion will remain central to the next generation of combustion devices that
are likely to employ blends of renewable and fossil fuels, transitioning eventually to …

Abstract Direct Numerical Simulations (DNS) are performed to investigate the process of
spontaneous ignition of hydrogen flames at laminar, turbulent, adiabatic and non-adiabatic …

This study demonstrates the stabilization of a sequential combustor with Nanosecond
Repetitively Pulsed Discharges (NRPD). Sequential combustors offer advantages such as …

This work uses multiple three-dimensional Direct Numerical Simulations (DNSs) to i)
investigate the ignition process of a cold lean premixed mixture at atmospheric conditions by …

Axial fuel staging enables elevation of the turbine inlet temperature in advanced heavy-duty
gas turbine combustors to∼ 2000 K, ultimately to achieve more than 65% combined cycle …

This article experimentally investigates the suppressing of combustion instability in a model
gas turbine combustor with annular air jets. Three parameters were optimized to find the …

Fundamental combustion characteristics of H 2/air flames with the addition of actual H 2/air
combustion residuals (a mixture of 65% N 2+ 35% H 2 O by mole) are examined …

We address the problem of turbulent spontaneous ignition vs. deflagration propagating
against a mean residence time gradient, particularly relevant to the stabilization of quasi …

The combustion regime transition in a sequential burner (SB) supplied with H 2 (48 kW) is
experimentally studied during steady and transient operation. The test rig is a simplified …

Combustion in hot and low oxygen environments—such as those encountered in practical
devices including inter-turbine burners and sequential gas turbines—is not yet fully …