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Volumn 3 PART A, Issue , 2006, Pages 547-556

The effects of obstructions on film cooling effectiveness on the suction side of a gas turbine vane

Author keywords

[No Author keywords available]

Indexed keywords

ADIABATIC EFFECTIVENESS; GAS TURBINE VANES; UPSTREAM OBSTRUCTIONS;

EID: 33750869024     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1115/GT2006-90577     Document Type: Conference Paper
Times cited : (15)

References (10)
  • 1
    • 84922374780 scopus 로고    scopus 로고
    • Effect of partial coating blockage on film cooling effectiveness
    • Bunker, R. S., 2000, "Effect of Partial Coating Blockage on Film Cooling Effectiveness" ASME Paper No. 2000-GT-0244.
    • (2000) ASME Paper No. 2000-GT-0244
    • Bunker, R.S.1
  • 3
    • 0036820858 scopus 로고    scopus 로고
    • Evaluation of pressure side film cooling with flow and thermal field measurements, part I: Showerhead effects
    • Cutbirth, J. M. and Bogard, D. G., 2002, "Evaluation of Pressure Side Film Cooling with Flow and Thermal Field Measurements, Part I: Showerhead Effects," ASME Journal of Turbomachinery, Vol. 124, pp. 670-677.
    • (2002) ASME Journal of Turbomachinery , vol.124 , pp. 670-677
    • Cutbirth, J.M.1    Bogard, D.G.2
  • 4
    • 1942489163 scopus 로고    scopus 로고
    • The effects of high mainstream turbulence and turbine vane film cooling on the dispersion of a simulated hot streak
    • Jenkins, S., Varadarajan, K., and Bogard, D.G., 2004, "The Effects of High Mainstream Turbulence and Turbine Vane Film Cooling on the Dispersion of a Simulated Hot Streak." ASME Journal of Turbomachinery, v 126, pp. 203-210.
    • (2004) ASME Journal of Turbomachinery , vol.126 , pp. 203-210
    • Jenkins, S.1    Varadarajan, K.2    Bogard, D.G.3
  • 6
    • 0035299266 scopus 로고    scopus 로고
    • Scaling of performance for varying density ratio coolants on an airfoil with strong curvature and pressure gradients
    • Ethridge, M. I., Cutbirth, J. M., and Bogard, D.G., 2001, "Scaling of Performance for Varying Density Ratio Coolants on an Airfoil with Strong Curvature and Pressure Gradients," ASME Journal of Turbomachinery, v. 123, pp. 231-237.
    • (2001) ASME Journal of Turbomachinery , vol.123 , pp. 231-237
    • Ethridge, M.I.1    Cutbirth, J.M.2    Bogard, D.G.3
  • 9
    • 27744456758 scopus 로고    scopus 로고
    • Degradation of film cooling performance on a turbine vane suction side due to surface roughness
    • Rutledge, J.L., Robertson, D.R., and Bogard, D.G, 2005, "Degradation of Film Cooling Performance on a Turbine Vane Suction Side Due to Surface Roughness," ASME paper GT2005-69045.
    • (2005) ASME Paper , vol.GT2005-69045
    • Rutledge, J.L.1    Robertson, D.R.2    Bogard, D.G.3


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.