Spray Characteristics of Simplex Swirl Injector with Low Hydrodynamic Disturbance Generated by Pressure Fluctuation in Feed Line

축방향 압력섭동에 의해 발생되는 저주파 수력학적 교란이 단일 스월 인젝터에 미치는 영향 분석

  • 길태옥 (서울대학교 기계항공공학부) ;
  • 김성혁 (서울대학교 기계항공공학부) ;
  • 김현성 (서울대학교 기계항공공학부) ;
  • 윤영빈 (서울대학교 기계항공공학부 항공우주신기술연구소)
  • Published : 2007.03.31

Abstract

The low frequency combustion instability phenomena generated by pressure drop oscillation such as propellant shake in feed line are studied. To generate the flowrate oscillation by the pressure pulsation up to 400Hz without flow discontinuities and cavitations, a hydrodynamic mechanical pulsator of rotating disk type was produced. Injection pressure conditions are 5, 7 and 9 bar and pressure fluctuation frequency conditions are 0, 4, 6 and 8 Hz. When the injection pressure was oscillated by a mechanical pulsator, the spray shape was pulsated regularly. During the pulsated state of the spray with a mechanical pulsator, the spray characteristics, such as spray angle and liquid film thickness in orifice exit, were measured and compared with those in steady state without a mechanical pulsator. Though the mean injection pressure was fixed in the steady and fluctuating state, there were some differences in all measured values, i.e. liquid film thickness and spray cone angle, between both states.

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