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Volumn 3, Issue , 2000, Pages

Aerodynamic loss characteristics of a turbine blade with trailing edge coolant ejection: Part 2 : External aerodynamics, total pressure losses and predictions

Author keywords

[No Author keywords available]

Indexed keywords

COMPUTATIONAL FLUID DYNAMICS; COOLANTS; FLOW FIELDS; FLOW VISUALIZATION; FLUID MECHANICS; HEAT TRANSFER; NAVIER STOKES EQUATIONS; REYNOLDS NUMBER; STREAM FLOW; TURBINE COMPONENTS; TURBINES; TURBOMACHINE BLADES; TURBULENCE MODELS; TURBULENT FLOW; VELOCITY MEASUREMENT; WAKES;

EID: 84961318974     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1115/2000-GT-0557     Document Type: Conference Paper
Times cited : (4)

References (12)
  • 1
    • 0346296635 scopus 로고    scopus 로고
    • The aerodynamics of trailing-edge-cooled transonic turbine blades: Part 1-experimental approach
    • Orlando, Florida, June 2-June 5, 1997. ASME Paper No: 97-GT-518
    • Deckers M., Denton J.D., 1997, "The Aerodynamics of Trailing-Edge-Cooled Transonic Turbine Blades: Part 1-Experimental Approach", Presented at the International Gas Turbine Institute & Aeroengine Congress & Exhibition, Orlando, Florida, June 2-June 5, 1997. ASME Paper No: 97-GT-518
    • (1997) Presented at the International Gas Turbine Institute & Aeroengine Congress & Exhibition
    • Deckers, M.1    Denton, J.D.2
  • 5
    • 0030462679 scopus 로고    scopus 로고
    • Aerodynamic performance of a transonic turbine guide vane with trailing edge coolant ejection: Part 1-experimental approach
    • Kapteijn C., Amecke J., Michelassi V., 1996, "Aerodynamic Performance of a Transonic Turbine Guide Vane with Trailing Edge Coolant Ejection: Part 1-Experimental Approach", Journal of Turbomachinery, Vol. 118, pp. 519-528.
    • (1996) Journal of Turbomachinery , vol.118 , pp. 519-528
    • Kapteijn, C.1    Amecke, J.2    Michelassi, V.3
  • 6
    • 0030398791 scopus 로고    scopus 로고
    • Performance analysis of a turbine stage having cooled nozzle blades with trailing edge ejection
    • November 5-7, 1996 Jakarta, Indonesia. ASME paper No: 96-TA-12
    • Kim J.H., Kim T.S., Lee J.S., Ro S.T., 1996, "Performance Analysis of a Turbine Stage Having Cooled Nozzle Blades with Trailing Edge Ejection", Presented at the 1996 ASME Turbo Asia Conference, November 5-7, 1996, Jakarta, Indonesia. ASME paper No: 96-TA-12
    • (1996) Presented at the 1996 ASME Turbo Asia Conference
    • Kim, J.H.1    Kim, T.S.2    Lee, J.S.3    Ro, S.T.4
  • 9
    • 84926034162 scopus 로고
    • Techniques for aerodynamic loss measurement of transonic turbine cascades with trailing-edge region coolant ejection
    • Cologne, Germany, June 1-June 4, 1992. ASME Paper No: 92-GT-157
    • Mee D.J., 1992, "Techniques for Aerodynamic Loss Measurement of Transonic Turbine Cascades with Trailing-Edge Region Coolant Ejection", Presented at the International Gas Turbine Institute & Aeroengine Congress & Exhibition, Cologne, Germany, June 1-June 4, 1992. ASME Paper No: 92-GT-157
    • (1992) Presented at the International Gas Turbine Institute & Aeroengine Congress & Exhibition
    • Mee, D.J.1
  • 10
    • 77953625174 scopus 로고    scopus 로고
    • Optimization of trailing edge ejection mixing losses: A theoretical and experimental study
    • Orlando, Florida, June 2-June 5, 1997. ASME Paper No: 97-GT-523
    • Pappu K.R., Schobeiri M.T., 1997, "Optimization of Trailing Edge Ejection Mixing Losses: A Theoretical and Experimental Study", Presented at the International Gas Turbine Institute & Aeroengine Congress & Exhibition, Orlando, Florida, June 2-June 5, 1997. ASME Paper No: 97-GT-523
    • (1997) Presented at the International Gas Turbine Institute & Aeroengine Congress & Exhibition
    • Pappu, K.R.1    Schobeiri, M.T.2
  • 11
    • 0029673606 scopus 로고    scopus 로고
    • Investigation of the flow field downstream of a turbine trailing edge cooled nozzle guide vane
    • Sieverding C.H., Arts T., Dénos R., Martelli F., 1996, "Investigation of the Flow Field Downstream of a Turbine Trailing Edge Cooled Nozzle Guide Vane", Journal of Turbomachinery, Vol. 118, pp. 291-300.
    • (1996) Journal of Turbomachinery , vol.118 , pp. 291-300
    • Sieverding, C.H.1    Arts, T.2    Dénos, R.3    Martelli, F.4
  • 12
    • 84955278526 scopus 로고    scopus 로고
    • Aerodynamic loss characteristics of a turbine blade with trailing edge coolant ejection part 1: Effect of cut-back length, spanwise rib spacing, free stream reynolds number and chordwise rib length on discharge coefficients
    • Germany 8-11 May 2000
    • Uzol O., Camci C., Glezer B., 2000, "Aerodynamic Loss Characteristics of a Turbine Blade with Trailing Edge Coolant Ejection Part 1: Effect of Cut-Back Length, Spanwise Rib Spacing, Free Stream Reynolds Number and Chordwise Rib Length on Discharge Coefficients", Presented at the 45th ASME International Gas Turbine & Aeroengine Technical Congress, Exposition and Users Symposium Munich, Germany 8-11 May 2000
    • (2000) Presented at the 45th ASME International Gas Turbine & Aeroengine Technical Congress, Exposition and Users Symposium Munich
    • Uzol, O.1    Camci, C.2    Glezer, B.3


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.