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Volumn 122, Issue 2, 2000, Pages 348-359

A three-dimensional coupled internal/external simulation of a film-cooled turbine vane

Author keywords

[No Author keywords available]

Indexed keywords

COMPUTATIONAL FLUID DYNAMICS; COMPUTER SIMULATION; HEAT FLUX; HEAT TRANSFER COEFFICIENTS; NAVIER STOKES EQUATIONS; TURBINES;

EID: 0034177998     PISSN: 0889504X     EISSN: None     Source Type: Journal    
DOI: 10.1115/1.555450     Document Type: Conference Paper
Times cited : (86)

References (27)
  • 2
    • 0032124987 scopus 로고    scopus 로고
    • Adiabatic wall effectiveness measurements of film-cooling holes with expanded exits
    • Gritsch, M., Schulz., A., and Wittig, S., 1998, "Adiabatic Wall Effectiveness Measurements of Film-Cooling Holes With Expanded Exits," ASME J. Turbomach., 120, pp. 549-556.
    • (1998) ASME J. Turbomach. , vol.120 , pp. 549-556
    • Gritsch, M.1    Schulz, A.2    Wittig, S.3
  • 3
    • 11644284181 scopus 로고    scopus 로고
    • Flowfield measurements for film-cooling holes with expanded exits
    • Thole, K., Gritsch, M., Schulz, A., and Wittig, S., 1998, "Flowfield Measurements for Film-Cooling Holes With Expanded Exits," ASME J. Turbomach., 120, pp. 327-336.
    • (1998) ASME J. Turbomach. , vol.120 , pp. 327-336
    • Thole, K.1    Gritsch, M.2    Schulz, A.3    Wittig, S.4
  • 4
    • 0034070489 scopus 로고    scopus 로고
    • A detailed analysis of film-cooling physics: Part I - Streamwise injection with cylindrical holes
    • Walters, D. K., and Leylek, J. H., 2000, "A Detailed Analysis of Film-Cooling Physics: Part I - Streamwise Injection With Cylindrical Holes," ASME J. Turbomach., 122, pp. 102-112.
    • (2000) ASME J. Turbomach. , vol.122 , pp. 102-112
    • Walters, D.K.1    Leylek, J.H.2
  • 5
    • 0034077170 scopus 로고    scopus 로고
    • A detailed analysis of film cooling physics: Part II - Compound-angle injection with cylindrical holes
    • McGovern, K. T., and Leylek, J. H., 2000, "A Detailed Analysis of Film Cooling Physics: Part II - Compound-Angle Injection With Cylindrical Holes," ASME J. Turbomach., 122, pp. 113-121.
    • (2000) ASME J. Turbomach. , vol.122 , pp. 113-121
    • McGovern, K.T.1    Leylek, J.H.2
  • 6
    • 0034123047 scopus 로고    scopus 로고
    • A detailed analysis of film cooling physics: Part III - Streamwise injection with shaped holes
    • Hyams, D. G., and Leylek, J. H., 2000, "A Detailed Analysis of Film Cooling Physics: Part III - Streamwise Injection With Shaped Holes." ASME J. Turbomach., 122, pp. 122-132.
    • (2000) ASME J. Turbomach. , vol.122 , pp. 122-132
    • Hyams, D.G.1    Leylek, J.H.2
  • 7
    • 0034108018 scopus 로고    scopus 로고
    • A detailed analysis of film cooling physics: Part IV - Compound-angle injection with shaped holes
    • Brittingham, R. A., and Leylek, J. H., 2000, "A Detailed Analysis of Film Cooling Physics: Part IV - Compound-Angle Injection With Shaped Holes," ASME J. Turbomach., 122, pp. 133-145.
    • (2000) ASME J. Turbomach. , vol.122 , pp. 133-145
    • Brittingham, R.A.1    Leylek, J.H.2
  • 8
    • 0028465052 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 J. Turbomach., 116, pp. 358-368.
    • (1994) ASME J. Turbomach. , vol.116 , pp. 358-368
    • Leylek, J.H.1    Zerkle, R.D.2
  • 10
    • 0023828989 scopus 로고
    • Stagnation film cooling and heat transfer, including its effect within the hole pattern
    • Mick, W. J., and Mayle, R. E., 1988, "Stagnation Film Cooling and Heat Transfer, Including its Effect Within the Hole Pattern," ASME J. Turbomach., 110, pp. 66-72.
    • (1988) ASME J. Turbomach. , vol.110 , pp. 66-72
    • Mick, W.J.1    Mayle, R.E.2
  • 11
    • 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 J. Turbomach., 119, pp. 343-351.
    • (1997) ASME J. Turbomach. , vol.119 , pp. 343-351
    • Garg, V.K.1    Gaugler, R.E.2
  • 22
    • 0032194622 scopus 로고    scopus 로고
    • Effect of squealer tip on rotor heat transfer and efficiency
    • Ameri, A., Rigby, D. L., and Steinthorsson, E., 1998. "Effect of Squealer Tip on Rotor Heat Transfer and Efficiency," ASME J. Turbomach., 120, pp. 753-759.
    • (1998) ASME J. Turbomach. , vol.120 , pp. 753-759
    • Ameri, A.1    Rigby, D.L.2    Steinthorsson, E.3
  • 24
    • 0028372478 scopus 로고
    • Simulation of transition with a two-equation turbulence model
    • Wilcox, D. C., 1994, "Simulation of Transition With a Two-Equation Turbulence Model," AIAA J., 32, No. 2, pp. 247-255.
    • (1994) AIAA J. , vol.32 , Issue.2 , pp. 247-255
    • Wilcox, D.C.1


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.