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Volumn 29, Issue 2, 2000, Pages 117-129

Aerodynamic performance of an annular cascade of film cooled nozzle guide vanes under engine representative conditions

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Indexed keywords


EID: 0000202677     PISSN: 07234864     EISSN: None     Source Type: Journal    
DOI: 10.1007/s003489900062     Document Type: Article
Times cited : (77)

References (24)
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  • 3
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    • Konsistente Mittelwerte in der Theorie der Turbomaschinen für Kompressible Medien
    • Dzung LS (1971) Konsistente Mittelwerte in der Theorie der Turbomaschinen für Kompressible Medien. BBC-Mitt. 58: 485-492
    • (1971) BBC-Mitt. , vol.58 , pp. 485-492
    • Dzung, L.S.1
  • 10
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    • Aerodynamic loss penalty produced by film cooling transonic turbine blades
    • Haller BR; Camus JJ (1984) Aerodynamic loss penalty produced by film cooling transonic turbine blades. J Eng for Gas Turbines and Power 106: 198-205
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  • 11
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    • Prediction of effects of mass-transfer cooling on the blade-row efficiency of turbine airfoils
    • San Diego, California, Jan 17-19
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    • (1972) AIAA Paper No 72-11 AIAA Aerospace Sciences Meeting
    • Hartsel, J.E.1
  • 12
    • 0023324597 scopus 로고
    • Influence of freestream turbulence and blade pressure gradient on boundary layer and loss behaviour of turbine cascades
    • Hoheisel H; Kiock R; Lichtfuss HJ; Fottner L (1987) Influence of freestream turbulence and blade pressure gradient on boundary layer and loss behaviour of turbine cascades. J Turbomachinery 109: 210-219
    • (1987) J Turbomachinery , vol.109 , pp. 210-219
    • Hoheisel, H.1    Kiock, R.2    Lichtfuss, H.J.3    Fottner, L.4
  • 13
    • 0019076037 scopus 로고
    • Aerodynamic loss in a gas turbine stage with film cooling
    • Ito S; Eckert ER; Goldstein RJ (1980) Aerodynamic loss in a gas turbine stage with film cooling. J Eng for Power 102: 964-970
    • (1980) J Eng for Power , vol.102 , pp. 964-970
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  • 14
    • 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; Michaelassi V (1996) Aerodynamic performance of a transonic turbine guide vane with trailing edge coolant ejection: Part 1 - Experimental approach. J Turbomachinery 118: 519-528
    • (1996) J Turbomachinery , vol.118 , pp. 519-528
    • Kapteijn, C.1    Amecke, J.2    Michaelassi, V.3
  • 19
    • 0030215802 scopus 로고    scopus 로고
    • Calibration of a four-hole pyramid probe and area traverse measurements in a short-duration transonic turbine cascade tunnel
    • Main AJ; Day CRB; Lock GD; Oldfield MLG (1996) Calibration of a four-hole pyramid probe and area traverse measurements in a short-duration transonic turbine cascade tunnel. Exp in Fluids 21: 302-311
    • (1996) Exp in Fluids , vol.21 , pp. 302-311
    • Main, A.J.1    Day, C.R.B.2    Lock, G.D.3    Oldfield, M.L.G.4
  • 20
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    • Free vortex theory for efficiency calculations from annular cascade data
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    • (1996) J Turbomachinery , vol.118 , pp. 291-300
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  • 24
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    • The use of foreign gas to simulate the effects of density ratios in film cooling
    • Teekaram AJH; Forth CJP; Jones TV (1989) The use of foreign gas to simulate the effects of density ratios in film cooling. J Turbomachinery 111: 57-62
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    • Teekaram, A.J.H.1    Forth, C.J.P.2    Jones, T.V.3


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.