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Volumn 3, Issue , 1997, Pages

Adiabatic wall effectiveness measurements of film-cooling holes with expanded exits

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; AIRCRAFT ENGINES; COOLANTS; GAS TURBINES; HEAT TRANSFER; MACH NUMBER;

EID: 84973640813     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1115/97-GT-164     Document Type: Conference Paper
Times cited : (14)

References (17)
  • 1
    • 84973667636 scopus 로고    scopus 로고
    • Film-cooling from holes with expanded exits: A comparison of computational results with experiment
    • Accepted for presentation at the Orlando, Florida, USA, June 2-5, 1997
    • Giebert, D., M. Gritsch, A. Schulz, and S. Wittig (1997). Film-Cooling from Holes with Expanded Exits: A Comparison of Computational Results with Experiment. Accepted for presentation at the 42nd Annual International Gas Turbine and Aeroengine Congress and Exposition, Orlando, Florida, USA, June 2-5, 1997.
    • (1997) 42nd Annual International Gas Turbine and Aeroengine Congress and Exposition
    • Giebert, D.1    Gritsch, M.2    Schulz, A.3    Wittig, S.4
  • 2
    • 0016061470 scopus 로고
    • Effects of hole geometry and density on three-dimensional film cooling
    • Goldstein, R., E. Eckert, and F. Burggraf (1974). Effects of Hole Geometry and Density on Three-Dimensional Film Cooling. Int. J. Heat Mass Transfer, Vol. 17, pp. 595-607.
    • (1974) Int. J. Heat Mass Transfer , Issue.17 , pp. 595-607
    • Goldstein, R.1    Eckert, E.2    Burggraf, F.3
  • 3
    • 84973598672 scopus 로고    scopus 로고
    • Discharge coefficient measurements of film-cooling holes with expanded exits
    • Accepted for presentation at the Orlando, Florida, USA, June 2-5, 1997
    • Gr tsch, M., A. Schulz, and S. Wittig (1997). Discharge Coefficient Measurements of Film-Cooling Holes with Expanded Exits. Accepted for presentation at the 42nd Annual International Gas Turbine and Aeroengine Congress and Exposition, Orlando, Florida, USA, June 2-5, 1997.
    • (1997) 42nd Annual International Gas Turbine and Aeroengine Congress and Exposition
    • Grtsch, M.1    Schulz, A.2    Wittig, S.3
  • 6
    • 0020736845 scopus 로고
    • Effect of crossflows on the discharge coefficient of film cooling holes
    • Hay, N., D. Lampard, and S. Benmansour (1983). Effect of Crossflows on the Discharge Coefficient of Film Cooling Holes . ASME Journal of Engineering for Power, Vol. 105, pp. 243-248.
    • (1983) ASME Journal of Engineering for Power , vol.105 , pp. 243-248
    • Hay, N.1    Lampard, D.2    Benmansour, S.3
  • 7
    • 0016432272 scopus 로고
    • Experimental investigation of film cooling with ejection from a row of holes for the application to gas turbine blades
    • Liess, C. (1975). Experimental Investigation of Film Cooling With Ejection From a Row of Holes for the Application to Gas Turbine Blades. ASME Journal of Engineering for Power, Vol. 97, pp. 21-27.
    • (1975) ASME Journal of Engineering for Power , vol.97 , pp. 21-27
    • Liess, C.1
  • 9
  • 14
    • 85007691353 scopus 로고
    • A study of the interaction of gaseous jets from transverse slots with supersonic external flows
    • Spaid, F. and E. Zukoski (1968). A Study of the Interaction of Gaseous Jets from Transverse Slots with Supersonic External Flows. AIAA Journal, Vol. 6, pp. 205-212.
    • (1968) AIAA Journal , vol.6 , pp. 205-212
    • Spaid, F.1    Zukoski, E.2
  • 16
    • 0031233658 scopus 로고    scopus 로고
    • Effect of a crossflow at the entrance to a film-cooling hole
    • Accepted for publication in the
    • Thole, K., M. Gritsch, A. Schulz, and S. Wittig (1997). Effect of a Crossflow at the Entrance to a Film- Cooling Hole. Accepted for publication in the ASME Journal of Fluids Engineering.
    • (1997) ASME Journal of Fluids Engineering
    • Thole, K.1    Gritsch, M.2    Schulz, A.3    Wittig, S.4


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.