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Volumn 6 B, Issue , 2003, Pages 999-1008

Interaction of labyrinth seal leakage flow and main flow in an axial turbine

Author keywords

[No Author keywords available]

Indexed keywords

MACH NUMBER; PITCH ANGLE; SECONDARY FLOWS;

EID: 0346335223     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1115/GT2003-38722     Document Type: Conference Paper
Times cited : (29)

References (21)
  • 1
    • 0346578354 scopus 로고    scopus 로고
    • An experimental investigation into the three-dimensional flow field and loss mechanisms in a two-stage axial turbine
    • C557/039/99, The 3rd European Conference on Turbomachinery, London
    • Breisig, V., Lerner, C., Peters, P., Pfost, H., Deckers, M., 1999, An experimental investigation into the three-dimensional flow field and loss mechanisms in a two-stage axial turbine, ImechE conference transactions, Turbomachinery Volume A, C557/039/99, pp. 33-42 The 3rd European Conference on Turbomachinery, London.
    • (1999) ImechE Conference Transactions, Turbomachinery , vol.A , pp. 33-42
    • Breisig, V.1    Lerner, C.2    Peters, P.3    Pfost, H.4    Deckers, M.5
  • 3
    • 0347839434 scopus 로고    scopus 로고
    • Experimental examination of the stator flow in a 1.5-stage axial turbine test stand
    • ATI-CST-013/01, The 4th European Conference on Turbomachinery, Firenze
    • Breisig, V., Giboni, A., Lerner, C., Peters, P., Pfost, H., 2001, Experimental examination of the stator flow in a 1.5-stage axial turbine test stand, ImechE conference transactions, pp. 179-188, ATI-CST-013/01, The 4th European Conference on Turbomachinery, Firenze.
    • (2001) ImechE Conference Transactions , pp. 179-188
    • Breisig, V.1    Giboni, A.2    Lerner, C.3    Peters, P.4    Pfost, H.5
  • 4
    • 0027677224 scopus 로고
    • The 1993 IGTI Scholar Lecture: Loss Mechanisms in Turbomachines
    • Denton, J. D., 1993, The 1993 IGTI Scholar Lecture: Loss Mechanisms in Turbomachines, Journal of Turbomachinery, Vol. 115, No. 4, pp 621-656.
    • (1993) Journal of Turbomachinery , vol.115 , Issue.4 , pp. 621-656
    • Denton, J.D.1
  • 8
    • 0029163709 scopus 로고
    • The Flow in a Second-Stage Nozzle of a Low-Speed Axial Turbine and its Effect on Tip Clearance Loss Development
    • Morphis, G., Bindon, J. P., 1995, The Flow in a Second-Stage Nozzle of a Low-Speed Axial Turbine and its Effect on Tip Clearance Loss Development, Journal of Turbomachinery, Vol. 117, No. 4, pp 571-577.
    • (1995) Journal of Turbomachinery , vol.117 , Issue.4 , pp. 571-577
    • Morphis, G.1    Bindon, J.P.2
  • 9
    • 84955093356 scopus 로고    scopus 로고
    • The Influence of the Clearance of Shrouded Rotor Blades on the Development of the Flowfield and Losses in the Subsequent Stator
    • 2000-GT-478, The 45th ASME International Gas Turbine & Aeroengine Technical Congress, Munich
    • Peters, P., Breisig, V., Giboni, A., Lerner, C., Pfost, H., 2000, The Influence of the Clearance of Shrouded Rotor Blades on the Development of the Flowfield and Losses in the Subsequent Stator, ASME Paper 2000-GT-478, The 45th ASME International Gas Turbine & Aeroengine Technical Congress, Munich.
    • (2000) ASME Paper
    • Peters, P.1    Breisig, V.2    Giboni, A.3    Lerner, C.4    Pfost, H.5
  • 11
    • 84955078887 scopus 로고    scopus 로고
    • Flow Interaction from the Exit Cavity of an Axial Turbine Blade Row Labyrinth Seal
    • 2000-GT-481
    • Pfau, A., Treiber, M., Sell, M., Gyarmathy G., 2000, Flow Interaction from the Exit Cavity of an Axial Turbine Blade Row Labyrinth Seal, ASME-Paper 2000-GT-481.
    • (2000) ASME-paper
    • Pfau, A.1    Treiber, M.2    Sell, M.3    Gyarmathy, G.4
  • 18
    • 84938924067 scopus 로고
    • Advanced Labyrinth Seal Design Performance for High Pressure Ratio Gas Turbines
    • Stocker, H. L., 1975, Advanced Labyrinth Seal Design Performance for High Pressure Ratio Gas Turbines, ASME-Paper 75-WA/GT-22.
    • (1975) ASME-paper 75-WA/GT-22
    • Stocker, H.L.1
  • 19
    • 0019073724 scopus 로고
    • Incompressible Flow in a Labyrinth Seal
    • Stoff, H., 1980, Incompressible Flow in a Labyrinth Seal, Journal of Fluid Mechanics, Vol. 100, pp 817-829.
    • (1980) Journal of Fluid Mechanics , vol.100 , pp. 817-829
    • Stoff, H.1
  • 20
    • 84955327526 scopus 로고    scopus 로고
    • The Control of Shroud Leakage Flows to Reduce Aerodynamic Losses in a Low Aspect Ratio, Shrouded Axial Flow Turbine
    • 2000-GT-475
    • Wallis, A. M., Denton, J. D., Demargne, A. A. J., 2000, The Control of Shroud Leakage Flows to Reduce Aerodynamic Losses in a Low Aspect Ratio, Shrouded Axial Flow Turbine, ASME-Paper 2000-GT-475.
    • (2000) ASME-paper
    • Wallis, A.M.1    Denton, J.D.2    Demargne, A.A.J.3
  • 21
    • 0026850014 scopus 로고
    • Influence of High Rotational Speeds on the Heat Transfer and Discharge Coefficients in Labyrinth Seals
    • Waschka, W., Wittig, S., Kim, S., 1992, Influence of High Rotational Speeds on the Heat Transfer and Discharge Coefficients in Labyrinth Seals, Journal of Turbomachinery, Vol. 114, No 2, pp462-468.
    • (1992) Journal of Turbomachinery , vol.114 , Issue.2 , pp. 462-468
    • Waschka, W.1    Wittig, S.2    Kim, S.3


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.