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Volumn 3, Issue , 1999, Pages

Film cooling effectiveness in the showerhead region of a gas turbine vane Part I: Stagnation region and near-pressure side

Author keywords

[No Author keywords available]

Indexed keywords

COAL FUELED GAS TURBINES; COOLANTS; COOLING; GAS TURBINES; HEAT TRANSFER; TURBOMACHINERY; TURBULENCE;

EID: 84928501121     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1115/99-GT-048     Document Type: Conference Paper
Times cited : (27)

References (11)
  • 1
    • 0030835581 scopus 로고    scopus 로고
    • Heat transfer and film cooling effectiveness in a linear airfoil cascade
    • Abuaf, N., Bunker, R., and Lee, C.F., 1997, "Heat Transfer and Film Cooling Effectiveness in a Linear Airfoil Cascade," Journal of Turbomachinery, Vol. 119, pp. 302-309.
    • (1997) Journal of Turbomachinery , vol.119 , pp. 302-309
    • Abuaf, N.1    Bunker, R.2    Lee, C.F.3
  • 2
    • 0032194331 scopus 로고    scopus 로고
    • Aspects of vane film cooling with high turbulence: Part ii - Adiabatic effectiveness
    • 1998
    • Ames, RE., 1998, "Aspects of Vane Film Cooling with High Turbulence: Part II - Adiabatic Effectiveness." Journal of Turbomachinery, Vol. 120, pp. 777-784, 1998.
    • (1998) Journal of Turbomachinery , vol.120 , pp. 777-784
    • Ames, R.E.1
  • 3
    • 0031381410 scopus 로고    scopus 로고
    • Experimental and numerical conjugate flow and heat transfer investigation of a shower-head cooled turbine guide vane
    • Bohn, D.E., Becker, V.J., and Rungen, AU., 1997, "Experimental and Numerical Conjugate Flow and Heat Transfer Investigation of a Shower-Head Cooled Turbine Guide Vane," ASME Paper No. 97-GT-15.
    • (1997) ASME Paper No. 97-GT-15
    • Bohn, D.E.1    Becker, V.J.2    Rungen, A.U.3
  • 4
    • 0031360624 scopus 로고    scopus 로고
    • The influence of coolant supply geometry on the film cooling exit flow and surface adiabatic effectiveness
    • Burd, S.W. and Simon, T.W. 1997, "The Influence of Coolant Supply Geometry on the Film Cooling Exit Flow and Surface Adiabatic Effectiveness." ASME Paper No. 97-GT-25.
    • (1997) ASME Paper No. 97-GT-25
    • Burd, S.W.1    Simon, T.W.2
  • 5
    • 0031342441 scopus 로고    scopus 로고
    • Investigation of various parametric influences on leading edge film cooling
    • Cruse, M.W., Yulci, U.M., Bogard, D.G., 1997, "Investigation of Various Parametric Influences on Leading Edge Film Cooling," ASME Paper No. 97-GT-296.
    • (1997) ASME Paper No. 97-GT-296
    • Cruse, M.W.1    Yulci, U.M.2    Bogard, D.G.3
  • 6
    • 0024866421 scopus 로고
    • Isothermal flow in a gas turbine combustor - A benchmark experimental study
    • Kuotmos, P. and McQuirk, J.J. 1989, "Isothermal Flow in a Gas Turbine Combustor - A Benchmark Experimental Study." Experiments in Fluids. Vol. 7, pp. 344-354.
    • (1989) Experiments in Fluids , vol.7 , pp. 344-354
    • Kuotmos, P.1    McQuirk, J.J.2
  • 11
    • 84928501122 scopus 로고    scopus 로고
    • Film cooling effectiveness in the showerhead region of a gas turbine vane part 11: Stagnation region and near-suction side
    • Indianapolis
    • Witteveld, V.C., Polanka, M.D., and Bogard, D.G., 1999, "Film Cooling Effectiveness in the Showerhead Region of a Gas Turbine Vane Part 11: Stagnation Region and Near-Suction Side," submitted to the ASME IGT1 Conference, Indianapolis.
    • (1999) Submitted to the ASME IGT1 Conference
    • Witteveld, V.C.1    Polanka, M.D.2    Bogard, D.G.3


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.