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1
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0346296635
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The aerodynamics of trailing-edge-cooled transonic turbine blades: Part 1-experimental approach
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Orlando, Florida, June 2-June 5, 1997. ASME Paper No: 97-GT-518
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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
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(1997)
Presented at the International Gas Turbine Institute & Aeroengine Congress & Exhibition
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Deckers, M.1
Denton, J.D.2
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4
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0022247281
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NASA Technical Memorandum 86900
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Hippensteele S.A., Russell L.M., Torres F.J., 1985, "Local Heat Transfer Measurements on a Large, Scale-Model Turbine Blade Airfoil Using a Composite of a Heater Element and Liquid Crystals", NASA Technical Memorandum 86900
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(1985)
Local Heat Transfer Measurements on A Large, Scale-Model Turbine Blade Airfoil Using A Composite of A Heater Element and Liquid Crystals
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Hippensteele, S.A.1
Russell, L.M.2
Torres, F.J.3
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5
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0030462679
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Aerodynamic performance of a transonic turbine guide vane with trailing edge coolant ejection: Part 1-experimental approach
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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.
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(1996)
Journal of Turbomachinery
, vol.118
, pp. 519-528
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Kapteijn, C.1
Amecke, J.2
Michelassi, V.3
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6
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0030398791
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Performance analysis of a turbine stage having cooled nozzle blades with trailing edge ejection
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November 5-7, 1996 Jakarta, Indonesia. ASME paper No: 96-TA-12
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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
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(1996)
Presented at the 1996 ASME Turbo Asia Conference
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Kim, J.H.1
Kim, T.S.2
Lee, J.S.3
Ro, S.T.4
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7
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0004312231
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Aerodynamic effect of coolant ejection in the rear part of transonic rotor blades
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Kost F.H., Holmes A.T., 1985, "Aerodynamic Effect of Coolant Ejection in the Rear Part of Transonic Rotor Blades", AGARD Conference Proceedings No. 390, Heat Transfer and Cooling in Gas Turbines, pp. 41-1-41-12.
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(1985)
AGARD Conference Proceedings 390, Heat Transfer and Cooling in Gas Turbines
, pp. 411-4112
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Kost, F.H.1
Holmes, A.T.2
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9
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84926034162
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Techniques for aerodynamic loss measurement of transonic turbine cascades with trailing-edge region coolant ejection
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Cologne, Germany, June 1-June 4, 1992. ASME Paper No: 92-GT-157
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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
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(1992)
Presented at the International Gas Turbine Institute & Aeroengine Congress & Exhibition
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Mee, D.J.1
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10
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77953625174
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Optimization of trailing edge ejection mixing losses: A theoretical and experimental study
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Orlando, Florida, June 2-June 5, 1997. ASME Paper No: 97-GT-523
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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
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(1997)
Presented at the International Gas Turbine Institute & Aeroengine Congress & Exhibition
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Pappu, K.R.1
Schobeiri, M.T.2
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11
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0029673606
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Investigation of the flow field downstream of a turbine trailing edge cooled nozzle guide vane
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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.
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(1996)
Journal of Turbomachinery
, vol.118
, pp. 291-300
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Sieverding, C.H.1
Arts, T.2
Dénos, R.3
Martelli, F.4
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12
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84955278526
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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
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Germany 8-11 May 2000
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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
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(2000)
Presented at the 45th ASME International Gas Turbine & Aeroengine Technical Congress, Exposition and Users Symposium Munich
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Uzol, O.1
Camci, C.2
Glezer, B.3
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