비대칭분류의 노즐출구영역에서의 난류유동장 해석

The Near Field Structure of Initially Asymmetic Jets

  • 김경훈 (경희대학교 기계.산업시스템 공학부, 레이저공학 연구소) ;
  • 신정관 (경희대학교 대학원 기계공학과, (주)센추리 중앙연구소) ;
  • 이한영 (오산대학 기계공학과)
  • 발행 : 1999.12.31

초록

The near field structure of round turbulent jets with initially asymmetric velocity distribution is investigated experimentally. Experiments were carried out using a constant temperature hot-wire anemometry system to measure streamwise velocity in the jets. The measurements were undertaken across the jet at various streamwise stations in a range starting from the jet exit plane and up to a downstream location of twelve diameters. The experimental results include the distribution of mean and instantaneous velocities, vorticity field, turbulence intensity, and the Reynolds shear stress. The asymmetry of the jet exit plane was obtained by using circular cross-section pipes with a bend at the upstream of the exit. Three pipes were used for this study: A straight pipe, 90 and 160 degree-bended pipes. Therefore, at the upstream of the pipe exit, the secondary flow through the bend and the mean streamwise velocity distribution could be controlled by changing the curvature of pipes.

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