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0002045812
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Film cooling in the presence of mainstream pressure gradients
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The two-dimensional behaviour of film cooling jets on concave surfaces
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Heat transfer and film cooling effectiveness in a linear airfoil cascade
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Abuaf, N., Bunker, R., Lee, C.P., 1995, "Heat Transfer and Film Cooling Effectiveness in a Linear Airfoil Cascade", ASME paper 95-GT-3
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Abuaf, N.1
Bunker, R.2
Lee, C.P.3
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6
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0031374946
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Flowfield measurements on a large scale turbine cascade with leading edge film cooling by two rows of holes
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Ardey, S., Fottner, L., 1997, "Flowfield Measurements on a Large Scale Turbine Cascade with Leading Edge Film Cooling by Two Rows of Holes", ASME paper 97-GT-524
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Ardey, S.1
Fottner, L.2
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7
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84905750021
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Pressure surface separations in low pressure turbines: Part 1 of 2 - Midspan Behaviour
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ASME Turbo Expo, New Orleans, Jun.
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Brear, MJ, Hodson, HP, Harvey, NW, 2001, "Pressure surface separations in low pressure turbines: Part 1 of 2 - Midspan Behaviour", ASME Paper No 2001-GT-0437, ASME Turbo Expo, New Orleans, Jun.
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Brear, M.J.1
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Harvey, N.W.3
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8
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84905757868
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Pressure surface separations in low pressure turbines: Part 2 of 2 -Interactions with the secondary flow
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ASME Turbo Expo, New Orleans, Jun.
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Brear, MJ, Hodson, HP, Gonzalez, P, Harvey, NW, 2001, "Pressure surface separations in low pressure turbines: Part 2 of 2 -Interactions with the secondary flow", ASME Paper No 2001-GT-0438, ASME Turbo Expo, New Orleans, Jun.
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Brear, M.J.1
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9
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84928551805
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The secondary flow field of a turbine cascade with 3D airfoil design and endwall contouring at off-design incidence
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Indianapolis 1999 (Trans. ASME)
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Duden, A.; Fottner, L., 1997, "The Secondary Flow Field of a Turbine Cascade with 3D Airfoil Design and Endwall Contouring at Off-Design Incidence", ASME Paper 99-GT-211, Indianapolis 1999 (Trans. ASME)
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Duden, A.1
Fottner, L.2
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10
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0032855270
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Controlling the secondary flow in a turbine cascade by three-dimensional airfoil design and endwall contouring
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11
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0032818719
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Measurement and calculation of nozzle guide vane end wall
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Harvey, N.W.; Rose, M.G.; Coupland, J.; Jones, T.V.: Measurement and Calculation of Nozzle Guide Vane End Wall Heat Transfer J. Turbom., 121, 1999 (Ts.ASME), S. 184-190
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12
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0032702073
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Heat transfer and flow field measurements in the leading edge region of a stator vane endwall
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Trans.ASME
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Kang, M.B.; Kohli, A.; Thole, K.A.: Heat Transfer and Flow field Measurements in the Leading Edge Region of a Stator Vane Endwall J. Turbomachinery, 121, 1999 (Trans.ASME), S. 558-568
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13
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84928494182
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Flowfield measurements in the endwall region of a stator vane
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Indianapolis (Trans.ASME)
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Kang, M.B.; Thole, K.A.: Flowfield Measurements in the Endwall Region of a Stator Vane ASME Paper 99-GT-188, Indianapolis 1999 (Trans.ASME)
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Kang, M.B.1
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14
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0030195489
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Rhode, Johnson, Broussard, Younger, Wernig, "Flow Visualization and Leackage Measurements of Stepped Labyrinth Seals, Part 1&2", 1996, ASME Paper No. 96-GT-136/137
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Rhode1
Johnson2
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17
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0003993318
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CFD analysis of dual spool turbine configuration
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24
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26
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4043162690
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Entwicklung eines Verfahrens zur Generierung vollständig parametrisierter, dreidimensionaler CFD-Rechengitter am Beispiel konvektivfilmgekühlter Turbinenschaufelhinterkanten
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Martini, P.1
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Wittig, S.3
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28
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0037002849
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Numerical investigation of heat transfer in turbine cascades with separated flows
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De la Calzada, P., Alonso, A.,2002, "Numerical Investigation of Heat Transfer in Turbine Cascades with Separated Flows", ASME paper GT-2002-30225
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De La Calzada, P.1
Alonso, A.2
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29
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0346335571
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Experimental and numerical investigation of trailing edge film cooling by circular coolant wall jets ejected from a slot with internal ribs
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GT2003-38157, Atlanta, USA, June 16-19
-
Martini, P., Schultz, A. & Wittig, S. Experimental and Numerical Investigation of Trailing Edge Film Cooling by Circular Coolant Wall Jets Ejected From a Slot with Internal Ribs, GT2003-38157, ASME/IGTI Turbo Expo 2003, Atlanta, USA, June 16-19, 2003.
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ASME/IGTI Turbo Expo 2003
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Martini, P.1
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Wittig, S.3
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30
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0348226265
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Heat transfer and pressure drop evaluation in thin wedge shaped trailing edge
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GT2003-38197, Atlanta, USA, June 16-19
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Carcasci, C.1
Facchini, B.2
Innocenti, L.3
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31
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10244243761
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Aero-thermodynamic aspects of film-cooling in regions on the pressure side of a high-lift blade
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submitted to the, Vienna, DRAFT GT2004-654067
-
Homeier, L., Lutum, E., Cunat, D., Janke, E., Haselbach, F., "Aero-Thermodynamic Aspects of Film-Cooling in Regions on the Pressure Side of a High-Lift Blade", submitted to the ASME/IGTI Turbo Expo 2004, Vienna, DRAFT GT2004-654067
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ASME/IGTI Turbo Expo 2004
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Homeier, L.1
Lutum, E.2
Cunat, D.3
Janke, E.4
Haselbach, F.5
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32
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10244276927
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Heat transfer analysis of a wedge shaped duct with pin fin and pedastal arrays: A comparison between numerical and experimental results
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submitted to the, Vienna, DRAFT GT2004-53319
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Antonio Andreini, Carlo Carcasci, Andrea Magi, "Heat transfer analysis of a wedge shaped duct with pin fin and pedastal arrays: A comparison between numerical and experimental results.", submitted to the ASME/IGTI Turbo Expo 2004, Vienna, DRAFT GT2004-53319
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ASME/IGTI Turbo Expo 2004
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Andreini, A.1
Carcasci, C.2
Magi, A.3
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33
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10244260459
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Pedestals and endwall contributions in heat transfer in a thin wedge shaped trailing edge
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submitted to the, Vienna, DRAFT GT2004-53152
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Bruno Facchini, Luca Innocenti, Lorenzo Tarchi, "Pedestals and endwall contributions in heat transfer in a thin wedge shaped trailing edge" submitted to the ASME/IGTI Turbo Expo 2004, Vienna, DRAFT GT2004-53152
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ASME/IGTI Turbo Expo 2004
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Facchini, B.1
Innocenti, L.2
Tarchi, L.3
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34
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10244274711
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Film Cooling in unsteady flow with separation bubble
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Muenchen
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M. Deinert and J. Hourmouziadis, "Film Cooling in unsteady flow with separation bubble,", DGLR Jahrestagung, Muenchen, 2003
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DGLR Jahrestagung
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Deinert, M.1
Hourmouziadis, J.2
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35
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10244221156
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Comparison of turbine tip leakage flow for flat tip and squealer tip geometroies at high-speed conditions
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submitted to the, Vienna, DRAFT GT2004-53979
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Nicole L. Ke, Tony Arts, "Comparison of turbine tip leakage flow for flat tip and squealer tip geometroies at high-speed conditions", submitted to the ASME/IGTI Turbo Expo 2004, Vienna, DRAFT GT2004-53979
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ASME/IGTI Turbo Expo 2004
-
-
Ke, N.L.1
Arts, T.2
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