This study deals with the experimental characterization of the induced flow dynamics by a
disk-needle-type plasma actuator driven by a sinusoidal generator and located in a …

Re-ignition of aeroengines under high altitude conditions is of great importance to the safety
and use of lean-burn flame. This study is focused on the experimental and numerical …

This study investigates the kinetic modeling of CH4/H2/Air mixture with nanosecond pulse
discharge (NSPD) by varying H2/CH4 ratios from 0 to 20% at ambient pressure and …

This study presents an experimental and numerical investigation on a surface sliding
discharge in a supersonic airflow in the presence of an oblique shock wave. In experiments …

Uncertainties are widely present in the design and simulation of aero-engine combustion
systems. Common non-probabilistic convex models are only capable of processing …

This study investigates the flame characterization near to lean blowout (LBO) limits at
different pre-heating temperatures in lifted swirl methane-air plasma discharge stabilized …

Re-ignition of aeroengine under high altitude conditions is of great importance to the safety
and use of lean-burn engines. The present work investigated the experimental and …

The lift-off phenomenon in turbulent jet flames has garnered significant attention, but it also
presents the risk of fuel leakage and flame blowout. Stabilizing flames remains a significant …

Due to its enhancement in the flame speed, ozone added in lean premixed syngas turbulent
jet flame was investigated by the three-dimensional direct numerical simulation method in …

The development of innovative aero-engine combustors has been devoted to drastically
reducing pollutants emissions and improving engine performances in recent years. These …