超音速气体雾化(ultra-sonic gas atomization,USGA))喷嘴是实现喷射雾化的重要装置,它能够产生脉动的超音速气流,获得较小的平均粒径和集中的粒径分布.在USGA喷嘴的共振管端部引入了主动的激励信号,组成双激励式超音速气体雾化器,并对...超音速气体雾化(ultra-sonic gas atomization,USGA))喷嘴是实现喷射雾化的重要装置,它能够产生脉动的超音速气流,获得较小的平均粒径和集中的粒径分布.在USGA喷嘴的共振管端部引入了主动的激励信号,组成双激励式超音速气体雾化器,并对超音速气体雾化器内部Hart-mann腔体气体流场在无激励/有激励情况下所产生的气体振动特性进行了数值研究.结果表明在主动激励器的作用下,超音速气体雾化器内气流的振动效果如振幅和起振特性等都得到了有效的加强.研究发现超音速气体雾化器存在多个气体受激振动的共振频率,其对应于两类不同的共振模式,"Hartmann模式"和"全局模式".双激励器信号的频率、激励幅度及相位差改变都能够有效地改变超音速气流的振动特性.研究同时阐明了Hartmann共振管和二次共振管在USGA喷嘴腔体内产生气体脉动时的联动特点.展开更多
The resonant behaviors of an ultra-sonic gas atomization nozzle with a zero mass-flux jet actuator were numerically investigated with FLUENT software by using a double precision unsteady two-dimensional pressure-based...The resonant behaviors of an ultra-sonic gas atomization nozzle with a zero mass-flux jet actuator were numerically investigated with FLUENT software by using a double precision unsteady two-dimensional pressure-based solver. The Spalart-Allmaras turbulence model was adopted in the simulations. Numerical results indicated that the oscillation properties of the gas efflux were effectively improved. Several resonatory frequencies corresponding to different vibration modes of gas were distinguished in the nozzle. With the changing of nozzle geometric parameters, different characters among those modes were elucidated by analyzing the propagations of pressure waves.展开更多
The gas flow in the Hartmann resonance tube is numerically investigated by the finite volume method based on the Roe solver. The oscillation of the flow is studied with the presence of a needle actuator set along the ...The gas flow in the Hartmann resonance tube is numerically investigated by the finite volume method based on the Roe solver. The oscillation of the flow is studied with the presence of a needle actuator set along the nozzle axis. Numerical results agree well with the theoretical and experimental results available. Numerical results indicate that the resonance mode of the resonance tube will switch by means of removing or adding the actuator. The gas flow in the ultrasonic gas atomization （USGA） nozzle is also studied by the same numerical methods. Oscillation caused by the Hartmann resonance tube structure, coupled with a secondary resonator, in the USGA nozzle is investigated. Effects of the variation of parameters on the oscillation are studied. The mechanism of the transition of subsonic flow to supersonic flow in the USGA nozzle is also discussed based on numerical results.展开更多
文摘超音速气体雾化(ultra-sonic gas atomization,USGA))喷嘴是实现喷射雾化的重要装置,它能够产生脉动的超音速气流,获得较小的平均粒径和集中的粒径分布.在USGA喷嘴的共振管端部引入了主动的激励信号,组成双激励式超音速气体雾化器,并对超音速气体雾化器内部Hart-mann腔体气体流场在无激励/有激励情况下所产生的气体振动特性进行了数值研究.结果表明在主动激励器的作用下,超音速气体雾化器内气流的振动效果如振幅和起振特性等都得到了有效的加强.研究发现超音速气体雾化器存在多个气体受激振动的共振频率,其对应于两类不同的共振模式,"Hartmann模式"和"全局模式".双激励器信号的频率、激励幅度及相位差改变都能够有效地改变超音速气流的振动特性.研究同时阐明了Hartmann共振管和二次共振管在USGA喷嘴腔体内产生气体脉动时的联动特点.
基金supported by the National Natural Science Foundation of China (Grant Nos.10772107, 10702038)the Shanghai Municipal Key Projects on Basic Research (Grant No.08JC1409800)+1 种基金the Innovation Project of Shanghai Municipal Education Commission (Grant No.08YZ10)the Shanghai Municipal Science and Technology Commission (Grant No.09DZ1141502)
文摘The resonant behaviors of an ultra-sonic gas atomization nozzle with a zero mass-flux jet actuator were numerically investigated with FLUENT software by using a double precision unsteady two-dimensional pressure-based solver. The Spalart-Allmaras turbulence model was adopted in the simulations. Numerical results indicated that the oscillation properties of the gas efflux were effectively improved. Several resonatory frequencies corresponding to different vibration modes of gas were distinguished in the nozzle. With the changing of nozzle geometric parameters, different characters among those modes were elucidated by analyzing the propagations of pressure waves.
文摘The gas flow in the Hartmann resonance tube is numerically investigated by the finite volume method based on the Roe solver. The oscillation of the flow is studied with the presence of a needle actuator set along the nozzle axis. Numerical results agree well with the theoretical and experimental results available. Numerical results indicate that the resonance mode of the resonance tube will switch by means of removing or adding the actuator. The gas flow in the ultrasonic gas atomization （USGA） nozzle is also studied by the same numerical methods. Oscillation caused by the Hartmann resonance tube structure, coupled with a secondary resonator, in the USGA nozzle is investigated. Effects of the variation of parameters on the oscillation are studied. The mechanism of the transition of subsonic flow to supersonic flow in the USGA nozzle is also discussed based on numerical results.
