Film Cooling from Two Rows of Holes with Opposite Orientation Angles : Heat Transfer

    • AHN Joon
    • School of Mech. and Aerospace Eng., Seoul National Univ.
    • JUNg In sung
    • School of Mech. and Aerospace Eng., Seoul National Univ
    • LEE Joon Sik
    • School of Mech. and Aerospace Eng., Seoul National Univ..

Abstract

Heat transfer coefficient ratio distributions are measured for film cooling from two rows of holes with opposite orientation angles. The inclination angle is fixed at 35゜, and orientation angles are set to 45゜ for the downstream row and -45゜ for the upsteam row. Four film cooling hole arrangements including inline and staggered configurations are investigated. The blowing ratios considered are 0.5, 1.0 and Configuration effects on the heat transfer are not significant at the blowing ratio of 0.5. At the higher blowing ratios of 1.0 and 2.0, however, the inline configuration produces higher heat transfer coefficient distributions compared to others. In spite of the high heat transfer level, the inline configuration shows better film cooling performance, represented by the heat flux ratio, at the blowing rations of 1.0 and 2.0 due to its higher adiabatic film cooling effectiveness.

Journal

JSME international journal. Ser. B, Fluids and thermal engineering   [List of Volumes]

JSME international journal. Ser. B, Fluids and thermal engineering 43(4), 706-711, 2000-11-15  [Table of Contents]

The Japan Society of Mechanical Engineers

References:  7

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Codes

  • NII Article ID (NAID) :
    110003474400
  • NII NACSIS-CAT ID (NCID) :
    AA10888815
  • Text Lang :
    ENG
  • Article Type :
    ART
  • ISSN :
    13408054
  • NDL Article ID :
    5586715
  • NDL Source Classification :
    ZN11(科学技術--機械工学・工業)
  • NDL Call No. :
    Z53-Y271
  • Databases :
    CJP  NDL  NII-ELS