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1
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0013329187
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Distribution of film-cooling effectiveness on a turbine endwall measured using the ammonia and diazo technique
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ASME Paper 95-GT-1
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Visualization study of three-dimensional flows in a turbine cascade endwall region
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Kawai, T.1
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4
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Turbulent transport on the endwall in the region between adjacent turbine blades
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6
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0013329041
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Three-dimensional flow near the blade/endwall junction of a gas turbine: Application of a boundary layer fence
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7
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Burd, S.W.1
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9
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0004350590
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Measurements over a film-cooled contoured endwall with various injection rates
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ASME Paper No. 2001-GT-140
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Oke, R.A.1
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10
-
-
4243511849
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Secondary flow reduction in a nozzle vane cascade by non-axisymmetric endwall profiling
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ASME Paper 99-GT-339
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11
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0003992010
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Non-axisymmetric endwall profiling in a turbine rotor blade
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12
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0003572078
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13
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84885315804
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ASME Paper 00-GT-0199
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14
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84885315804
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ASME Paper 00-GT-0200
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15
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84925870512
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Reduction in secondary flows and losses in a turbine cascade by upstream boundary layer blowing
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ASME Paper 93-GT-114
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16
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0004238102
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Prediction and measurement of film cooling effectiveness for a first-stage turbine vane shroud
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17
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0037898796
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Roy, R.P., Squires, K.D., Gerendas, M., and Song, S., 2000 "Flow and Heat Transfer at the Hub Endwall of Inlet Vane Passages-Experiments and Simulations," ASME Paper No. 00-GT-198.
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Roy, R.P.1
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0003516627
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Wang, L. 1996 "A Study on Gas Turbine Flows, Turbulence Generation, and Film Cooling Flow Measurements," M.S. Thesis, Department of Mechanical Engineering, University of Minnesota.
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20
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84885307396
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Measurements in a gas turbine cascade with film cooling and endwall contouring
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Ph.D. Thesis, Department of Mechanical Engineering, University of Minnesota
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Oke, R.A., 2001 "Measurements in a Gas Turbine Cascade with Film Cooling and Endwall Contouring," Ph.D. Thesis, Department of Mechanical Engineering, University of Minnesota.
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21
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0002477246
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Describing uncertainties in single sample experiments
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