• Title/Summary/Keyword: 분무선단 궤적

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Correlations of Trajectory and Break-up Point for Liquid Jet Injected into Low Speed Cross-flow (저속 횡단유동장에 분사된 액체제트의 분무궤적 및 분열점에 대한 상관관계식)

  • Kim, Jong-Hyun;Lee, Bong-Soo;Koo, Ja-Ye
    • Journal of ILASS-Korea
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    • v.13 no.2
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    • pp.79-84
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    • 2008
  • The correlations for cross-flow have not been well established, because of the complexity of breakup and atomization mechanism. A study was performed to investigate the characteristics of spray behaviour of liquid jet in the bag breakup regime injected into low-speed cross-flow with the pressure single-hole nozzle. The shadow-graphy method was used for the cross-flow jet visualization. The experimental variables of liquid jet were nozzle diameter $(0.3mm{\sim}1.0mm)$, injection pressure $(50kPa{\sim}150kPa)$, and the velocity of cross-flow $(27m/s{\sim}42m/s)$. The highest penetration trajectories of liquid jet are governed by the momentum ratio $({\rho}_{\iota}U_{\iota}^2/{\rho}_aU_{cross}^2)$ rather than the Weber number and the new empirical equations of the highest penetration trajectory and breakup point at low-speed corss-flow are established.

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Characteristics of SMD and Volume Flux of Two-phase Jet Injected into Cross-flow with Various Gas-liquid Ratio and Reynolds Number (횡단 유동장의 기액비 및 레이놀즈수 변화에 따른 외부혼합형 이상유체 제트의 액적크기 및 체적유속 특성)

  • Kim, Jong-Hyun;Lee, Bong-Soo;Koo, Ja-Ye
    • Transactions of the Korean Society of Automotive Engineers
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    • v.17 no.2
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    • pp.75-81
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    • 2009
  • A study was performed to investigate the characteristics of two-phase jet injected into subsonic cross-flow using the external mixed gas blast two-phase nozzle. The shadowgraph method was adopted for the cross-flow jet visualization and PDPA system was used to measure droplet size, velocity, and volume flux. The atomization of two-phase jet is initially determined according to gas to liquid mass flow-rate ratio and the Reynolds number of cross-flows. The highest penetration trajectories of two-phase jet injected into cross-flow are governed by the momentum ratio at subsonic cross-flow. As GLR of two-phase jet injected into cross-flow increases, the droplet size decreases and the distribution area of volume flux increases. The distribution of volume flux that influenced by the counter vortex pair at the downstream of cross-flow is symmetric in shape of horseshoe.