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Effect of Flare Angle in Counter-Rotating Swirler on Swirling Flow

동축 반전 스월러의 플레어 각도변화가 스월러 유동에 미치는 영향 연구

  • 김택현 (과학기술연합대학원대학교 무기체계공학과) ;
  • 김성돈 ((주)터보헤드) ;
  • 진유인 (국방과학연구소 제4기술연구본부) ;
  • 민성기 (국방과학연구소 제4기술연구본부)
  • Received : 2016.02.05
  • Accepted : 2016.02.29
  • Published : 2016.03.30

Abstract

Swirler generates the overall swirling flow in the combustion chamber and this swirling flow governs the flame stability and enhances fuel atomization. This paper deals with the flare angle effects on flow streamlines, recirculation zone, Central Toroidal Recirculation Zone(CTRZ) and Corner Recirculation Zone(CRZ) in the model combustion chamber using counter-rotating swirler. 2D PIV system was employed to obtain the velocity components and test condition was obtained using Reynolds Analogy equivalent to air test. We observed transitional flow patterns of flare angle increased. The obtained results show that the flare angle controls the behavior of Recirculation zone, Central Toroidal Recirculation Zone and Corner Recirculation Zone.

Keywords

References

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