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Volumn 122, Issue 2, 2000, Pages 340-347

Unsteady wake effect on film temperature and effectiveness distributions for a gas turbine blade

Author keywords

[No Author keywords available]

Indexed keywords

BOUNDARY LAYER FLOW; GAS TURBINES; HEAT TRANSFER COEFFICIENTS; LIQUID CRYSTALS; REYNOLDS NUMBER; TRANSITION FLOW; TURBOMACHINE BLADES; UNSTEADY FLOW; WAKES;

EID: 0034176407     PISSN: 0889504X     EISSN: None     Source Type: Journal    
DOI: 10.1115/1.555457     Document Type: Conference Paper
Times cited : (60)

References (18)
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  • 3
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  • 6
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    • The influence of density difference between hot and coolant gas on film cooling by a row of holes: Predictions and experiments
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  • 7
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    • Ames, F. E., 1998, "Aspects of Vane Film Cooling With High Turbulence: Part I - Heat Transfer; Part II - Adiabatic Effectiveness," ASME J. Turbomach., 120, pp. 768-784.
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    • Ames, F.E.1
  • 8
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    • Abhari, R. S., and Epstein, A. H., 1994, "An Experimental Study of Film Cooling in a Rotating Transonic Turbine," ASME J. Turbomach., 116, pp. 63-70.
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  • 10
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    • (1994) ASME J. Turbomach. , vol.116 , pp. 730-737
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  • 12
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  • 13
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    • (1997) ASME J. Turbomach. , vol.119 , Issue.3 , pp. 587-593
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  • 14
    • 0032194349 scopus 로고    scopus 로고
    • Effect of unsteady wake on detailed heat transfer coefficient and film effectiveness distributions for a gas turbine blade
    • Du, H., Han, J. C., and Ekkard, S. V., 1998, "Effect of Unsteady Wake on Detailed Heat Transfer Coefficient and Film Effectiveness Distributions for a Gas Turbine Blade," ASME J. Turbomach., 120, pp. 808-817.
    • (1998) ASME J. Turbomach. , vol.120 , pp. 808-817
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  • 15
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    • Du, H., Ekkad, S. V., and Han, J., 1999, "Effect of Unsteady Wake With Trailing Edge Coolant Ejection on Film Cooling Performance for a Gas Turbine Blade," ASME J. Turbomach., 121, pp. 448-453.
    • (1999) ASME J. Turbomach. , vol.121 , pp. 448-453
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  • 16
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  • 17
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  • 18
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    • Aug. 23-28, Kyongju, Korea
    • Sohm, D. K., Teng, S., and Han, J. C., 1998, "Film Temperature and Effectiveness Measurements on a Cylindrical Leading Edge Film Cooling Model," Heat Transfer 1998, Proc. of 11th IHTC, 6, pp. 571-576, Aug. 23-28, Kyongju, Korea.
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* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.