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

An experimental investigation of flame structure, stability, and emissions performance was
conducted in a two-stage lab-scale generic combustor design operated with CH 4, H 2⁠ …

The air-assisted atomizer used in a two-stroke aviation engine has two separate operation
sequences, namely the fuel injection and air injection, in contrast to the synchronous fuel/air …

This paper investigates the formation of nitric oxide (NO) and carbon monoxide (CO)
emissions as a function of nitrogen (N 2) or carbon dioxide (CO 2) diluent content, added to …

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 …

The transverse injection of rich, premixed natural gas and air (NG-air) and natural gas,
hydrogen, and air (NG-H 2-air) reacting jets into a high-speed vitiated crossflow was …

The present paper numerically studies the impact of three gaseous fuels on the reaction
characteristics and pollutant formation in a lean combustion system. The models include an …

The present work explores a novel flow-independent liquid injection scheme, incorporating
solid obstructions to alter the key mechanisms controlling the liquid breakup and trajectory …

Liquid fuel jet in crossflow (LJIC) is a vital atomization technique significant to the aviation
industry. The hydrodynamic instability mechanisms that drive a primary breakup of a …

The effects of hydrogen enrichment and premixing on the emissions of a high-pressure
axially staged combustion system are experimentally and theoretically examined. The …