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Volumn 119, Issue 4, 1997, Pages 777-785

A systematic computational methodology applied to a three-dimensional film-cooling flowfield

Author keywords

[No Author keywords available]

Indexed keywords

COOLING; FLOW FIELD; GAS TURBINE;

EID: 0031441576     PISSN: 0889504X     EISSN: 15288900     Source Type: Journal    
DOI: 10.1115/1.2841188     Document Type: Article
Times cited : (143)

References (22)
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    • Andreopoulos, J.1    Rodi, W.2
  • 2
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    • “The Near-Field Character of a Jet Discharged Normal to a Main Stream
    • Bergeles, G., Gosman, A. D., and Launder, B. E., 1976, “The Near-Field Character of a Jet Discharged Normal to a Main Stream,” ASME Journal of Heat Transfer, Vol. 107, pp. 373-378.
    • (1976) ASME Journal of Heat Transfer , vol.107 , pp. 373-378
    • Bergeles, G.1    Gosman, A.D.2    Launder, B.E.3
  • 3
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    • Bergeles, G., Gosman, A. D., and Launder, B. E., 1977, “The Near-Field Character of a Jet Discharged Through a Wall at 30° to a Mainstream,” AIAA Journal, Vol. 14, pp. 499-504.
    • (1977) AIAA Journal , vol.14 , pp. 499-504
    • Bergeles, G.1    Gosman, A.D.2    Launder, B.E.3
  • 4
    • 0000976375 scopus 로고
    • The Turbulent Jet in a Cross Stream at Low Injection Rates: A Three-Dimensional Numerical Treatment
    • Bergeles, G., Gosman, A. D., and Launder, B. E., 1978, “The Turbulent Jet in a Cross Stream at Low Injection Rates: A Three-Dimensional Numerical Treatment,” Numerical Heat Transfer, Vol. 1, pp. 217-242.
    • (1978) Numerical Heat Transfer , vol.1 , pp. 217-242
    • Bergeles, G.1    Gosman, A.D.2    Launder, B.E.3
  • 6
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    • 1995, personal communications
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    • (1992)
    • Crawford, M.E.1
  • 9
    • 0030853358 scopus 로고    scopus 로고
    • Effect of Velocity and Temperature Distribution at the Hole Exit on Film Cooling of Turbine Blades
    • Garg, V. K., and Gaugler, R. E., 1997, “Effect of Velocity and Temperature Distribution at the Hole Exit on Film Cooling of Turbine Blades,” ASME Journal of Turbomachinery, Vol. 119, pp. 343-351.
    • (1997) ASME Journal of Turbomachinery , vol.119 , pp. 343-351
    • Garg, V.K.1    Gaugler, R.E.2
  • 13
    • 0018480361 scopus 로고
    • A Stable and Accurate Convection Modeling Procedure Based on Quadratic Upstream Interpolation
    • Leonard, B. P., 1979, “A Stable and Accurate Convection Modeling Procedure Based on Quadratic Upstream Interpolation,” Computer Methods in Applied Mechanics and Engineering, Vol. 19, pp. 59-98.
    • (1979) Computer Methods in Applied Mechanics and Engineering , vol.19 , pp. 59-98
    • Leonard, B.P.1
  • 14
    • 84925859797 scopus 로고
    • Discrete-Jet Film Cooling: A Comparison of Computational Results With Experiments
    • Leylek, J. H., and Zerkle, R. D., 1994, “Discrete-Jet Film Cooling: A Comparison of Computational Results With Experiments,” ASME Journal of Turbomachinery, Vol. 113, pp. 358-368.
    • (1994) ASME Journal of Turbomachinery , vol.113 , pp. 358-368
    • Leylek, J.H.1    Zerkle, R.D.2
  • 17
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    • Effects of Density Ratio on the Hydrodynamics of Film Cooling
    • Pietrzyk, J. R., Bogard, D. G., and Crawford, M. E., 1990, “Effects of Density Ratio on the Hydrodynamics of Film Cooling,” ASME Journal of Turbomachinery, Vol. 1 12, pp. 437-443.
    • (1990) ASME Journal of Turbomachinery , vol.1 , Issue.12 , pp. 437-443
    • Pietrzyk, J.R.1    Bogard, D.G.2    Crawford, M.E.3
  • 18
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  • 19
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  • 20
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    • Sinha, A. K., Bogard, D. G„ and Crawford, M. E., 1991, “Film Cooling Effectiveness Downstream of a Single Row of Holes With Variable Density Ratio,” ASME Journal of Turbomachinery, Vol. 113, pp. 442-449.
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    • Sinha, A.K.1    Bogard, D.G.2    Crawford, M.E.3


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.