Abstract: A planejet flame was manipulated by passing the fuel jet through a jetimpingement fluidic oscillator. The plane fuel jet bifurcated into two streams of selfsustained pulsating jets in the cavity of the fluidic oscillator ...

Abstract: The flame behavior and the thermal structure of gaseous fuel jets issued from rectangular nozzles of high and low aspect ratios with co-flowing air were experimentally studied. Two rectangular nozzles with aspect ratios ...

Abstract: The effects of acoustic excitation at resonance on the flame appearances, flame lengths, flame temperatures, and combustion product concentrations of combusting swirling dual-disk double-concentric jets were studied. The ...

Abstract: In the design of gas turbine combustors, efforts are engineered toward reducing the combustion pollutant emission levels. The pollutant emissions can be reduced by premixing the fuel and the air prior to ignition. However, ...

Abstract: The characteristic flow behavior, timeaveraged velocity distributions, phaseresolved ensembleaveraged velocity profiles, and turbulence properties of the flow in the interdisk midplane between shrouded two corotating disks ...

Abstract: To analyze the influence of hydrous ethanol on the performance of the direct-injection engine, the three-dimensional simulation is carried out by using converge software coupled with the combustion mechanism of hydrous ...