期刊文献+

Disintegration Process and Performance of a Coaxial Porous Injector 被引量:1

Disintegration Process and Performance of a Coaxial Porous Injector
原文传递
导出
摘要 In order to understand the breakup performance of coaxial porous injectors,the sprays of coaxial porous injectors with two different porous material cylinder lengths were compared with those of conventional shear coaxial injectors.To allow comparison,the wall injection lengths were designed to be equivalent to the value of the recess depth.Cold flow sprays were visualized using back-lit photography methods and analyzed quantitatively with a laser diffraction apparatus,in order to study the effects of the momentum flux ratio and Weber number on the breakup for each type of injector.In case of the shear coaxial injector,the large liquid core was observed in low air mass flow rate condition.However,the destabilization of the liquid jet from the coaxial porous injector is almost complete within the inner region,near the injector face plate.Additionally,better breakup performance in low gas flow rate condition was obtained when the porous cylinder length decreased,while the shear coaxial injectors showed better breakup efficiency when the recess length increased.In conclusion,the different breakup process caused by the radial momentum in the inner region of the porous injector disintegrated the liquid core. In order to understand the breakup performance of coaxial porous injectors,the sprays of coaxial porous injectors with two different porous material cylinder lengths were compared with those of conventional shear coaxial injectors.To allow comparison,the wall injection lengths were designed to be equivalent to the value of the recess depth.Cold flow sprays were visualized using back-lit photography methods and analyzed quantitatively with a laser diffraction apparatus,in order to study the effects of the momentum flux ratio and Weber number on the breakup for each type of injector.In case of the shear coaxial injector,the large liquid core was observed in low air mass flow rate condition.However,the destabilization of the liquid jet from the coaxial porous injector is almost complete within the inner region,near the injector face plate.Additionally,better breakup performance in low gas flow rate condition was obtained when the porous cylinder length decreased,while the shear coaxial injectors showed better breakup efficiency when the recess length increased.In conclusion,the different breakup process caused by the radial momentum in the inner region of the porous injector disintegrated the liquid core.
出处 《Journal of Thermal Science》 SCIE EI CAS CSCD 2016年第5期394-401,共8页 热科学学报(英文版)
基金 supported by a National Research Foundation of Korea(NRF)grant funded by the Korean Government(Ministry of Science,ICT and Future Planning)(No.NRF-2012M 1A3A3A02033146 and NRF-2013RlA5A1073861 through the SPRC of Seoul National University)
关键词 多孔喷嘴 同轴 性能 破碎效率 崩解 喷油器 喷射器 多孔材料 Coaxial porous injector Sauter mean diameter Droplet size distribution
  • 相关文献

参考文献1

二级参考文献16

  • 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.

共引文献1

同被引文献5

引证文献1

相关作者

内容加载中请稍等...

相关机构

内容加载中请稍等...

相关主题

内容加载中请稍等...

浏览历史

内容加载中请稍等...
;
使用帮助 返回顶部