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 …

High-spatiotemporal-resolution diagnostics are important for capturing fine physicochemical
structures in supersonic combustion. In this study, a high-speed camera (HSC)/dual …

Increasingly stringent regulations of pollutant emissions from aviation require rapid
implementation of novel combustion technologies. Promising concepts based on moderate …

In the present work, direct numerical simulation of a laboratory-scale lean premixed reacting
jet in cross-flow was performed to explore the flow–flame structures and turbulence–flame …

The utilization of syngas is crucial for reducing carbon emissions. When the reacting jet in
crossflow (RJICF) achieves moderate or intense low-oxygen dilution (MILD) combustion, it …

In this work, we perform an experimental study of the combustion of pure hydrogen in the
sequential stage of a generic combustor. This academic test rig is a simplified model of an …

In the present work, lean premixed jet flames in crossflow were studied using direct
numerical simulation to explore the effects of Damköhler numbers (D a) on turbulence and …