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Volumn 3 B, Issue , 2002, Pages 993-1001

Combustor turbine interface studies - Part 1: Endwall effectiveness measurements

Author keywords

[No Author keywords available]

Indexed keywords

COMBUSTOR TURBINE INTERFACE; ENDWALL EFFECTIVENESS MEASUREMENT; FILM COOLING;

EID: 0036994481     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1115/GT2002-30526     Document Type: Conference Paper
Times cited : (16)

References (15)
  • 1
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    • Langston, L.S.1
  • 2
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    • An experimental study of heat transfer and film cooling on large-scale turbine endwalls
    • November
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    • Blair, M.F.1
  • 3
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    • Prediction and measurement of film cooling effectiveness for a first-stage turbine vane shroud
    • 90-GT-95
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    • (1990)
    • Granser, D.1    Schulenberg, T.2
  • 4
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    • Effects of slot bleed ijection over a contoured endwall on nozzle guide vane cooling performance: Part I: Flow field measurements
    • ASME Paper No. 2000-GT-199
    • Burd, S. W. and Simon, T. W., "Effects of Slot Bleed Ijection over a Contoured Endwall on Nozzle Guide Vane Cooling Performance: Part I: Flow Field Measurements," ASME Paper No. 2000-GT-199.
    • Burd, S.W.1    Simon, T.W.2
  • 5
    • 79951737177 scopus 로고    scopus 로고
    • Effects of slot bleed ijection over a contoured endwall on nozzle guide vane cooling performance: Part II thermal measurements
    • 2000-GT-200
    • Burd, S. W., Satterness, C. J., and Simon, T. W., "Effects of Slot Bleed Ijection over a Contoured Endwall on Nozzle Guide Vane Cooling Performance: Part II Thermal Measurements," 2000-GT-200.
    • Burd, S.W.1    Satterness, C.J.2    Simon, T.W.3
  • 6
    • 0003414490 scopus 로고    scopus 로고
    • Measurements in a turbine cascade over a contoured endwall: Discrete hole injection of bleed flow
    • 2000-GT-214
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    • Oke, R.1    Simon, T.2    Burd, S.W.3    Vahlberg, R.4
  • 7
    • 0004350590 scopus 로고    scopus 로고
    • Measurements over a film-cooled, contoured endwall with various coolant injection rates
    • 2001-GT-140
    • Oke, R., Simon, T., Shih, T., Zhu, B., Lin, Y. L., Chyu, M. "Measurements Over a Film-Cooled, Contoured Endwall with Various Coolant Injection Rates," 2001-GT-140.
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  • 8
    • 0035483150 scopus 로고    scopus 로고
    • Turbine nozzle endwall film cooling study using pressure-sensitive paint
    • Zhang, L. J. and Jaiswal, R. S., 2001, "Turbine Nozzle Endwall Film Cooling Study Using Pressure-Sensitive Paint," J of Turbomachinery, vol. 123, pp. 730-738.
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    • Zhang, L.J.1    Jaiswal, R.S.2
  • 9
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    • Flow and heat transfer at the hub endwall of inlet vane passages-experiments and simulations
    • 2000-GT-198
    • Roy, R. P., Squires, K. D., Gerendas, M., Song, S., Howe, W. J., and Ansari, A., "Flow and Heat Transfer at the Hub Endwall of Inlet Vane Passages-Experiments and Simulations," 2000-GT-198.
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  • 10
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    • Film-cooled turbine endwall in a transonic flow field: Part I - Aerodynamic measurements
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  • 11
    • 0035483103 scopus 로고    scopus 로고
    • Film-cooled turbine endwall in a transonic flow field: Part II - Heat transfer and film-cooling effectiveness measurements
    • Nicklas, M., 2001, "Film-Cooled Turbine Endwall in a Transonic Flow Field: Part II - Heat Transfer and Film-Cooling Effectiveness Measurements," J of Turbomachinery, vol. 123, pp. 720-729.
    • (2001) J of Turbomachinery , vol.123 , pp. 720-729
    • Nicklas, M.1
  • 12
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    • (2000) J of Turbomachinery , vol.122 , pp. 255-262
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  • 13
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    • 2001-GT-0170 (to appear in J Turbomachinery)
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    • (2001)
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  • 14
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  • 15
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    • (2001)
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* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.