Spray Plume Characteristics of Liquid Jets in Subsonic Crossflows

수직분사제트의 액적영역 분무특성에 대한 연구

  • 송진관 (서울대학교 기계항공공학부 대학원) ;
  • 안규복 (한국항공우주연구원) ;
  • 오정석 (서울대학교 기계항공공학부 대학원) ;
  • 윤영빈 (서울대학교 기계항공공학부)
  • Published : 2006.06.30

Abstract

The effect of internal liquid flow on spray plume characteristics was performed experimentally in subsonic cross flows. The injector internal flow was classified as three modes such as a normal, cavitation, and hydraulic flip. The objectives of the research are to investigate the effect of internal liquid flow on the spray plume characteristics and compare the trajectory of spray plume with previous works. The results suggest that the trajectory and width of spray plume can be correlated as a function of liquid/air momentum flux ratio(q), injector diameter and normalized distance from the injector exit(x/d). It's also found that the injector internal turbulence influences the spray plume characteristics significantly.

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