Droplet Sizes and Velocities from Single-Hole Nozzle in Transversing Subsonic Air-stream

아음속 횡단류에 수직 분사되는 분무의 액적크기 및 속도 분포 특성

  • 이인철 (한국항공대학교 대학원) ;
  • 조우진 (한국항공대학교 대학원) ;
  • 이봉수 (한국항공대학교 대학원) ;
  • 김종현 (경원전문대 자동차학과) ;
  • 구자예 (한국항공대학교 항공우주 및 기계공학부)
  • Published : 2007.04.26

Abstract

The spray plume characteristics of liquid water jet injected into subsonic cross-flow at 42 m/s were experimentally investigated. Nozzle has a 1.0 m diameter and L/D=5. Droplet sizes, velocities, volume flux were measured at each downstream area of the injector exit using phase Doppler particle anemometry. Measuring probe position is moved with 3-way transversing machine. Experimental results indicate that SMD is varied from 75 to $120{\mu}m$ distribution and it is uncertain layer structure. SMD peaks at the top of the spray plume. This phenomenon is related to the momentum exchange between column waves and cross-flow stream. Droplet vector velocities were varied from 11.5 to 33 m/s. A higher-velocity region can be identified in down edge region at Z/D : 40, 70 and 100. Lower-velocity region were observed on bottom position of the spray plume. Volume flux is a criterion to the droplet concentration. All volume flux distribution has a same structure that continuously decreases from the center region to the edge of the plume. Z/D : 20 is spatially less concentrated than in Z/D : 100.

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