Study on the Atomization Characteristics of a Counter-swirling Two-phase Atomizer with Variations of Swirl angle

역선회 이류체 미립화기의 선회각 변화에 따른 미립화 특성연구

  • 김남훈 (전북대학교 대학원) ;
  • 이삼구 (전북대학교 대학원) ;
  • 하만호 (전북대학교 대학원) ;
  • 노병준 (전북대학교 기계항공시스템공학부, 공업기술연구소) ;
  • 강신재 (전북대학교 기계항공시스템공학부, 공업기술연구소)
  • Published : 2001.06.27

Abstract

Experimental and analytical researches have been conducted on the twin-fluid atomizers for better droplet breakup during the past decades. But, the studies on the disintegration mechanism still present a great challenge to understand the drop behavior and breakup structure. In an effort to describe the aerodynamic behavior of the sprays issuing from the internal mixing counter-swirling nozzle, the spatial distribution of axial (U) radial (V) and tangential (W) components of droplet velocities are investigated across the radial distance at several axial locations of Z=30, 50, 80, 120 and 170mm, respectively. Experiments were conducted for the liquid flow rates which was kept constant at 7.95 g/s and the air injection pressures were varied from 20 kPa to 140 kPa. Counter-swirling internal mixing nozzles manufactured at angles of $15^{\circ},\;30^{\circ},\;45^{\circ}$ and $60^{\circ}$ the central axis with axi-symmetric tangential-drilled holes was considered. The distributions of velocities and turbulence intensities are comparatively analyzed. PDPA is installed to specify spray flows, which have been conducted along the axial downstream distance from the nozzle exit. Ten thousand of sampling data was collected at each point with time limits of 30 second. 3-D automatic traversing system is used to control the exact measurement. It is observed that the sprays with all swirl angle have the maximum SMD for on air injection pressure of 20 kPa and 140 kPa with centerline, respectively. The nozzle with swirl angle of $60^{\circ}$ has vest performance.

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