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Mixing Characteristics of Pulsed Air-assist Liquid Jet into an Internal Subsonic Cross-flow 被引量:3

Mixing Characteristics of Pulsed Air-assist Liquid Jet into an Internal Subsonic Cross-flow
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摘要 Penetration depth,spray dispersion angle,droplet sizes in breakup processes and atomization processes are very important parameters in combustor of air-breathing engine.These processes will enhance air/fuel mixing inside the combustor.Experimental results from the pulsed air-assist liquid jet injected into a cross-flow are investigated.And experiments were conducted to a range of cross-flow velocities from 42~136 m/s.Air is injected with 0~300kPa,with air-assist pulsation frequency of 0~20Hz.Pulsation frequency was modulated by solenoid valve.Phase Doppler Particle Analyzer(PDPA) was utilized to quantitatively measuring droplet characteristics.High-speed CCD camera was used to obtain injected spray structure.Pulsed air-assist liquid jet will offer rapid mixing and good liquid jet penetration.Air-assist makes a very fine droplet which generated mist-like spray.Pulsed air-assist liquid jet will introduce additional supplementary turbulent mixing and control of penetration depth into a cross-flow field.The results show that pulsation frequency has an effect on penetration,transverse velocities and droplet sizes.The experimental data generated in these studies are used for a development of active control strategies to optimize the liquid jet penetration in subsonic cross-flow conditions and predict combustion low frequency instability. Penetration depth, spray dispersion angle, droplet sizes in breakup processes and atomization processes are very important parameters in combustor of air-breathing engine. These processes will enhance air/fuel mixing inside the combustor. Experimental results from the pulsed air-assist liquid jet injected into a cross-flow are investigated. And experiments were conducted to a range of cross-flow velocities from 42-136 m/s. Air is injected with 0-300kPa, with air-assist pulsation frequency of 0-20Hz. Pulsation frequency was modulated by solenoid valve. Phase Doppler Particle Analyzer(PDPA) was utilized to quantitatively measuring droplet characteristics. High-speed CCD camera was used to obtain injected spray structure. Pulsed air-assist liquid jet will offer rapid mixing and good liquid jet penetration. Air-assist makes a very fine droplet which generated mist-like spray. Pulsed air-assist liquid jet will introduce additional supplementary turbulent mixing and control of penetration depth into a cross-flow field. The results show that pulsation frequency has an effect on penetration, transverse velocities and droplet sizes. The experimental data generated in these studies are used for a development of active control strategies to optimize the liquid jet penetration in subsonic cross-flow conditions and predict combustion low frequency instability.
出处 《Journal of Thermal Science》 SCIE EI CAS CSCD 2010年第2期136-140,共5页 热科学学报(英文版)
基金 supported by the Korea Research Foundation Grant funded by the Korean Government (MOEHRD,Basic Research Promotion Fund) (KRF-2007-D00084)
关键词 脉冲频率调制 空气进入 液体射流 混合特性 亚音速 横流 相位多普勒粒子分析仪 穿透深度 cross-flow penetration pulsed air-assist liquid jet pulsation frequency
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参考文献5

  • 1K. C. Lin, P. J. Kennedy, T. A. Jackson, "Spray Structures of Aerated-Liquid Jets in Subsonic Cross-flows," AIAA Meeting & Exhibit, Reno, NV, 8-11 January 2001.
  • 2Krebs, W., Flohr, P., Prade, B., and Hoffman, S., "Thermoacoustic Stability Chart for High Intensity Gas Turbine Combustion Systems," Combustion Science and Technology, Vol. 174, No. 7, pp. 99-128, 2002.
  • 3Ducruix, S., Schuller, T., Durox, D., and Candel, S., "Combustion Dynamics and Instabilities; Elementary Coupling and Driving Mechanisms," Journal of Propulsion and Power, Vol. 19, No. 5, pp. 722-734, 2003.
  • 4C. Ghenai, O.I. Smith, and A. Karagozian, "Acoustical Excitation of Buming Fuel Droplets," 39th AIAA Aerospace Sciences Meeting and Exhibit, Reno, NV, January 2001.
  • 5M. Y. Leong, Ct Vincent, McDonell, and Ct S. Samuelsen, "Mixing of an Airblast-Atomized Fuel Spray Injected a Cross-flow of Air," NASA/CR 2000-210467, UCIARTR-00-05, 2000.

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