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Volumn 3, Issue , 1999, Pages

Effects of orientation angles on film cooling over a flat plate: Boundary layer temperature distributions and adiabatic film cooling effectiveness

Author keywords

[No Author keywords available]

Indexed keywords

BOUNDARY LAYERS; GAS TURBINES; HEAT TRANSFER; LIQUID CRYSTALS; TEMPERATURE DISTRIBUTION; VELOCITY;

EID: 84928473687     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1115/99-GT-143     Document Type: Conference Paper
Times cited : (6)

References (11)
  • 1
    • 0025463235 scopus 로고
    • Behavior of a coolant film with two rows of holes along the pressure side of a high-pressure nozzle guide vane
    • Arts, T. and Bourguignon, A. E., 1990, "Behavior of a Coolant Film with Two Rows of Holes along the Pressure Side of a High-Pressure Nozzle Guide Vane," ASME Journal of Turbomachinvy, Vol. 112, pp. 512-521.
    • (1990) ASME Journal of Turbomachinvy , vol.112 , pp. 512-521
    • Arts, T.1    Bourguignon, A.E.2
  • 2
    • 0031191260 scopus 로고    scopus 로고
    • Film effectiveness over a flat surface with air and co2, injection through compound angle holes using a transient liquid crystal image method
    • Ekkad, S. V., Zapata, D. and Han,J. C., 1997, "Film Effectiveness over a Flat Surface with Air and CO2, Injection through Compound Angle Holes Using a Transient Liquid Crystal Image Method," ASME Journal of Turbomachinery, Vol. 119, pp.587-593.
    • (1997) ASME Journal of Turbomachinery , vol.119 , pp. 587-593
    • Ekkad, S.V.1    Zapata, D.2    Han, J.C.3
  • 5
    • 0028342198 scopus 로고
    • Behavior of the laterally injected jet in film cooling: Measurements of surface temperature and velocity/temperature field within the jet
    • Honami, S., Shizawa, T. and Uchiyama, A., 1994, "Behavior of the Laterally Injected Jet in Film Cooling: Measurements of Surface Temperature and Velocity/Temperature Field within the Jet," ASME Journal of Turbomachinely, Vol. 116, pp. 106-112.
    • (1994) ASME Journal of Turbomachinely , vol.116 , pp. 106-112
    • Honami, S.1    Shizawa, T.2    Uchiyama, A.3
  • 7
    • 0002477246 scopus 로고
    • Describing uncertainties in single sample experiments
    • Kline, S. J. and McClintock, F. A., 1953, "Describing Uncertainties in Single Sample Experiments," Mechanical Engineering, Vol. 75, pp. 3-8.
    • (1953) Mechanical Engineering , vol.75 , pp. 3-8
    • Kline, S.J.1    McClintock, F.A.2
  • 8
    • 0030751913 scopus 로고    scopus 로고
    • Flow characteristics and aerodynamic losses of film-cooling jets with compound angle orientations
    • Lee, S. W., Kim, Y. B. and Lee, J.S., 1997, "Flow Characteristics and Aerodynamic Losses of Film-Cooling Jets with Compound Angle Orientations," ASME Journal of Turbomachinery, Vol. 119, pp. 310-319.
    • (1997) ASME Journal of Turbomachinery , vol.119 , pp. 310-319
    • Lee, S.W.1    Kim, Y.B.2    Lee, J.S.3
  • 9
    • 21144462846 scopus 로고
    • Heat transfer, adiabatic effectiveness, and injectant distributions downstream of a single row and two staggered rows of compound angle film-cooling holes
    • Ligrani, P. M., Ciriello, S. and Bishop, D. T., 1992 "Heat Transfer, Adiabatic Effectiveness, and Injectant Distributions Downstream of a Single Row and Two Staggered Rows of Compound Angle Film-Cooling Holes," ASME Journal of Turbomachinery, Vol. 114, pp. 687-700.
    • (1992) ASME Journal of Turbomachinery , vol.114 , pp. 687-700
    • Ligrani, P.M.1    Ciriello, S.2    Bishop, D.T.3
  • 10
    • 85006265000 scopus 로고
    • Influence of high mainstream turbulence on leading edge film cooling heat transfer
    • Mehendale, A. B. and Han, J C., 1992, "Influence of High Mainstream Turbulence on Leading Edge Film Cooling Heat Transfer," ASME Journal of Turbomachinery, Vol. 114, pp. 707-715.
    • (1992) ASME Journal of Turbomachinery , vol.114 , pp. 707-715
    • Mehendale, A.B.1    Han, J.C.2
  • 11
    • 4243193913 scopus 로고    scopus 로고
    • Film cooling with compound angle holes: Adiabatic effectiveness
    • Schmidt, D. L., Sen, B. and Bogard, D. G., 1996, "Film Cooling with Compound Angle Holes: Adiabatic Effectiveness," ASME Journal of Turbomachinery, Vol. 118, pp. 807-813.
    • (1996) ASME Journal of Turbomachinery , vol.118 , pp. 807-813
    • Schmidt, D.L.1    Sen, B.2    Bogard, D.G.3


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.