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Volumn 121, Issue 2, 1999, Pages 225-232

Film cooling effectiveness and mass/heat transfer coefficient downstream of one row of discrete holes

Author keywords

[No Author keywords available]

Indexed keywords

FLOW MEASUREMENT; GAS TURBINES; HEAT TRANSFER; MASS TRANSFER; MEASUREMENT ERRORS; SUBLIMATION; THIN FILMS;

EID: 0032865196     PISSN: 0889504X     EISSN: 15288900     Source Type: Journal    
DOI: 10.1115/1.2841305     Document Type: Article
Times cited : (78)

References (17)
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  • 2
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    • Heat (Mass) Transfer and Film Cooling Effectiveness With Injection Through Discrete Holes: 1-Within Holes and on the Back Surface
    • Cho, H. H., and Goldstein, R. J., 1995a, “Heat (Mass) Transfer and Film Cooling Effectiveness With Injection Through Discrete Holes: 1-Within Holes and on the Back Surface,” ASME Journal of Turbomachinery, Vol. 117, pp. 440-450.
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  • 3
    • 0029155060 scopus 로고
    • Heat (Mass) Transfer and Film Cooling Effectiveness With Injection Through Discrete Holes: 2-On the Exposed Surface
    • Cho, H. H., and Goldstein, R. J., 1995b, “Heat (Mass) Transfer and Film Cooling Effectiveness With Injection Through Discrete Holes: 2-On the Exposed Surface,” ASME Journal of Turbomachinery, Vol. 117, pp. 451-460.
    • (1995) ASME Journal of Turbomachinery , vol.117 , pp. 451-460
    • Cho, H.H.1    Goldstein, R.J.2
  • 4
    • 0021190898 scopus 로고
    • Analysis of Film Cooling and Full-Coverage Film Cooling of Gas Turbine Blades, ASME
    • Eckert, E. R. G., 1984, “Analysis of Film Cooling and Full-Coverage Film Cooling of Gas Turbine Blades,” ASME Journal of Engineering for Gas Turbines and Power, Vol. 106, pp. 206-213.
    • (1984) Journal of Engineering for Gas Turbines and Power , vol.106 , pp. 206-213
    • Eckert, E.R.G.1
  • 5
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    • Film Effectiveness Over a Flat Surface With Air and C02 Injection Through Compound Angle Holes Using a Transient Liquid Crystal Image Method
    • 2 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
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  • 6
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  • 7
    • 0016058529 scopus 로고
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    • Eriksen, V. L., and Goldstein, R. J., 1974, “Heat Transfer and Film Cooling Following Injection Through Inclined Circular Tubes,” ASME Journal of Heat Transfer, Vol. 96, pp. 239-245.
    • (1974) Journal of Heat Transfer , vol.96 , pp. 239-245
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  • 8
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    • The Flow and Film Cooling Effectiveness Following Injection Through a Row of Holes, ASME
    • Foster, N. W., and Lampard, D., 1980, “The Flow and Film Cooling Effectiveness Following Injection Through a Row of Holes,” ASME Journal of Engineering for Power, Vol. 102, pp. 584-588.
    • (1980) Journal of Engineering for Power , vol.102 , pp. 584-588
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  • 10
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    • Goldstein, R. J., and Taylor, J. R., 1982, “Mass Transfer in the Neighborhood of Jets Entering Crossflow,” ASME Journal of Heat Transfer, Vol. 104, pp. 715-721.
    • (1982) ASME Journal of Heat Transfer , vol.104 , pp. 715-721
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  • 11
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    • A Review of Mass Transfer Measurements Using Naphthalene Sublimation
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  • 12
    • 0344603142 scopus 로고    scopus 로고
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    • Minneapolis, MN
    • Olson, R. L., 1996, “Film Cooling Effectiveness and Heat (Mass) Transfer Coefficient for a Single Row of Discrete Film Cooling Holes,” Master’s Thesis, University of Minnesota, Minneapolis, MN.
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  • 13
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    • Pedersen, D. R., Eckert, E. R. G., and Goldstein, R. J., 1977, “Film Cooling With Large Density Differences Between the Mainstream and the Secondary Fluid Measured by the Heat-Mass Transfer Analogy,” ASME Journal of Heat Transfer, Vol. 99, pp. 620-627.
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  • 14
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  • 15
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* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.