다중 오리피스 노즐을 이용한 충돌분류의 열전달 향상에 관한 실험적 연구

An experimental study on the heat transfer augmentation by using the multiple orifice nozzle

  • 김예용 (부산대학교 대학원 기계공학과) ;
  • 정기호 (부산대학교 대학원 항공우주공학) ;
  • 김귀순 (부산대학교 항공우주공학) ;
  • 서태범 (인하대학교 기계·항공·자동화 공학부)
  • 발행 : 1999.09.01

초록

An experimental study has been peformed to investigate the heat transfer characteristics of impinging jets with multiple orifice nozzles. Four different shapes of multiple orifice nozzle were tested to improve the heat transfer characteristics of impinging jet. Heat transfer coefficients were obtained by using transient and steady method based on the liquid crystal thermography, and both methods showed very similar results. The effects of multiple orifice nozzles on the heat transfer characteristics of impinging jets were discussed in detail. The results showed that multiple orifice nozzles improved the heat transfer characteristics of impinging jet. Especially, heat transfer coefficients around stagnation region of impinging jets were highly increased.

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