Heat transfer coefficient measurement in the Blockage channel with Repeated Jet Impingement

반복된 제트 충돌을 갖는 내부 유로의 평균 열전달 계수 측정

  • 박승덕 (한국항공대학교 항공우주 및 기계공학부) ;
  • 이기선 (한국항공대학교 항공우주 및 기계공학부) ;
  • 김석범 (한국항공대학교 항공우주 및 기계공학부) ;
  • 조용화 (한국항공대학교 항공우주 및 기계공학부) ;
  • 전창수 (한국항공대학교 항공우주 및 기계공학부) ;
  • 곽재수 (한국항공대학교 항공우주 및 기계공학부) ;
  • 허재성 (한국항공우주연구원 KHP 개발실)
  • Published : 2008.12.31

Abstract

Averaged heat transfer coefficients were measured in a turbine blade internal cooling passage model with three blockage walls. Each blockage wall was equipped with 9 staggered holes or slots in order to create different shaper of repeated jet impingement. The effect of jet shape on the averaged heat transfer coefficient was studied by the copper-thermocouple method and three Reynolds number of 10,000, 20,000, and 30,000 were tested. Results showed that the repeated stagger jets could increase the averaged heat transfer coefficient by at least 9 times compared to the smooth channel cases. Due to the large pressure drop induced by the repeated jet impingement, the thermal performance was less than 1 for all cases and decreased as the Reynolds number increased. Among the tested cases, the widest slot showed the best thermal performance. The measurement results showed that the thermal performance of the heat transfer augmentation by repeated stagger jets could be improved by altering the jet shape, and other shape of impingement jet will be studied in near future.

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