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Breakup Structure of Two-phase Jets with Various Momentum Flux from a Porous Injector 被引量:2

Breakup Structure of Two-phase Jets with Various Momentum Flux from a Porous Injector
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摘要 Spray structure and atomization characteristics were investigated through a comparison of a porous and a shear coaxial injector. The porous injector shows better atomization performance than the shear coaxial injector. To increase atomization performance and mixing efficiency of two-phase jets, a coaxial porous injector which can be applicable to liquid rocket combustors was designed and tested. The characteristics of atomization and spray from a porous and a shear coaxial injector were characterized by the momentum flux ratio. The breakup mechanism of the porous injector is governed by Taylor-Culick flow and axial shear forces. Momentum of injected gas flow through a porous material which is composed of sintered metal is radically transferred to the center of the liquid column, and then liquid column is effectively broken up. Although the shapes of spray from porous and shear coaxial jets were similar for various momentum ratio, spray structures such as spray angle and droplet sizes were different. As increasing the momentum flux ratio, SMD from the porous injector showed smaller value than the shear coaxial Spray structure and atomization characteristics were investigated through a comparison of a porous and a shear coaxial injector. The porous injector shows better atomization performance than the shear coaxial injector. To in- crease atomization performance and mixing efficiency of two-phase jets, a coaxial porous injector which can be applicable to liquid rocket combustors was designed and tested. The characteristics of atomization and spray from a porous and a shear coaxial injector were characterized by the momentum flux ratio. The breakup mechanism of the porous injector is governed by Taylor-Culick flow and axial shear forces. Momentum of injected gas flow through a porous material which is composed of sintered metal is radically transferred to the center of the liquid column, and then liquid column is effectively broken up. Although the shapes of spray from porous and shear co- axial jets were similar for various momentum ratio, spray structures such as spray angle and droplet sizes were different. As increasing the momentum flux ratio, SMD from the porous injector showed smaller value than the shear coaxial injector
出处 《Journal of Thermal Science》 SCIE EI CAS CSCD 2014年第1期60-67,共8页 热科学学报(英文版)
基金 supported by the National Research Foundation of Korea(NRF)grant funded by the Korean Government(MEST)(NRF-2011-0015435 and NRF-2012M 1A3A3A02033146)
关键词 多孔材料 动量通量 两相射流 喷油器 结构 通量分裂 同轴射流 雾化特性 Porous injector, Shear coaxial injector, Breakup mechanism, Momentum flux ratio
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  • 1Bazarov, V. G, "A New Class of Porous Injectors for Combustion Chambers and Gas Generator," 29th AIAA/ ASME/SAE/ASEE Joint Propulsion Conference & Ex- hibit 28-30 June, Monterey, CA, AIAA 93-1955, 1955.
  • 2Sozer, M., Shyy, W. and Thakur, S., "Multi-Scale Porous Media Modeling for Liquid Rocket Injector Applica- tions," 42nd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit 9-12 July, Sacramento, CA, AIAA 2006-5044, 2006.
  • 3Lux, J., Suslov, D. and Haidn, O., "Experimental Inves- tigation of Porous Injectors for Liquid Propellant Rocket Engines," 44th A/AA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit 21-23 July, Hartford, CT, AIAA 2008-4563, 2008.
  • 4Griffond, J. and Casalis, G., "Secondary Instability of the Planar Taylor Flow," 36th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, Huntsville, Alabama, AIAA 2000-3806, 2000.
  • 5Farago, Z., and Chigier, N., "Morphological Classifica- tion of Disintegration of Round Liquid Jets in a Coaxial Air Stream," Atomization and Sprays, Vol. 2, No. 2, pp. 137-153, 1992.
  • 6Lefebvre, A. H., "Twin-Fluid Atomization: Factors In- fluence Mean Drop Size," Atomization and Sprays, Vol. 2, No. 2, pp. 101-119, 1992.
  • 7Gautam, V. and Gupta, A.K., "Simulation of Mixing in Rocket Engine Injector under In-Space Conditions," 41st AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, Tucson, Arizona, AIAA 2005-1445, 2005.
  • 8Lasheras, J. C., ViUermaux, E. and Hopfmer, E. J., "Break-up and Atomization of a Round Water Jet by a High-speed Annular Air Jet," Journal of Fluid Mechanics,Vol. 357, pp. 351-379, 1998.
  • 9Rehap, H., Villermaux, E. and Hopfinger, E. J., "Flow Regimes of Large Velocity Ratio Coaxial Jets," Journal of Fluids Mechanics, Vol. 345, pp. 357-381, 1997.
  • 10Eroglu, H. and Chigier, N., "Initial Drop Size and Veloc- ity Distributions for Airblast Coaxial Atomizer," Journal of Fluids Engineering, Vol. 113, No.3, pp. 453--459, 1991.

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