GT2010-22270 A Numerical Study of an Impingement Array Inside a Three Dimensional Turbine Vane (English)
- New search for: De Paz, M.L.
- New search for: Jubran, B.A.
- New search for: De Paz, M.L.
- New search for: Jubran, B.A.
In:
ASME turbo expo
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101-112
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2010
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ISBN:
- Conference paper / Print
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Title:GT2010-22270 A Numerical Study of an Impingement Array Inside a Three Dimensional Turbine Vane
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Contributors:De Paz, M.L. ( author ) / Jubran, B.A. ( author ) / American Society of Mechanical Engineers; ASME International Gas Turbine Institute
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Conference:ASME turbo expo ; 2010 ; Glasgow
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Published in:ASME turbo expo ; 101-112PROCEEDINGS OF THE ASME TURBO EXPO ; 4a ; 101-112
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Publisher:
- New search for: ASME
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Place of publication:New York, N.Y.
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Publication date:2010-01-01
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Size:12 pages
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Remarks:Includes bibliographical references and author indexes
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ISBN:
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Type of media:Conference paper
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Type of material:Print
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Language:English
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Keywords:
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Source:
© Metadata Copyright the British Library Board and other contributors. All rights reserved.
Table of contents conference proceedings
The tables of contents are generated automatically and are based on the data records of the individual contributions available in the index of the TIB portal. The display of the Tables of Contents may therefore be incomplete.
- 1
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GT2010-22043 Experimental Investigation on Staggered Impingement Heat Transfer on a Rib Roughened Plate With Different Crossflow SchemesXing, Y. / Weigand, B. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 13
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GT2010-22139 An Experimental Study of Heat Transfer and Pressure Drop on the Bend Surface of a U-DuctSalameh, T. / Sunden, B. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 23
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GT2010-22173 Effects of a Realistically Rough Surface on Vane Aerodynamic Losses Including the Influence of Turbulence Condition and Reynolds NumberErickson, E.L. / Ames, F.E. / Bons, J.P. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 33
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GT2010-22174 Effects of a Realistically Rough Surface on Vane Heat Transfer Including the Influence of Turbulence Condition and Reynolds NumberErickson, E.L. / Ames, F.E. / Bons, J.P. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 43
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GT2010-22180 Flow and Heat Transfer of Air and Steam in Internal Cooling Passages of Turbine BladeWang, X. / Wang, W. / Chou, L. / Han, Y. / Xu, L. / Shui, L. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 53
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GT2010-22190 Influence of Channel Orientation on Heat Transfer in a Two-Pass Smooth and Ribbed Rectangular Channel (AR=2:1) Under Large Rotation NumbersHuh, M. / Lei, J. / Han, J.-C. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 67
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GT2010-22238 Model Verification of Mist/Steam Cooling With Jet Impingement Onto a Concave Surface and Prediction at Elevated Operating ConditionWang, T. / Dhanasekaran, T.S. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 81
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GT2010-22252 Heat Transfer Investigation of an Aggressive Intermediate Turbine Duct: Part 2-Numerical AnalysisWallin, F. / Osso, C.A. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 91
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GT2010-22265 Predictions of Enhanced Heat Transfer of an Internal Blade Tip-Wall With Hemispherical Dimples or ProtrusionsXie, G. / Sunden, B. / Wang, Q. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 101
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GT2010-22270 A Numerical Study of an Impingement Array Inside a Three Dimensional Turbine VaneDe Paz, M.L. / Jubran, B.A. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 113
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GT2010-22273 Effect of Turning Vane Configurations on Heat Transfer and Pressure Drop in a Ribbed Internal Cooling SystemChen, W. / Ren, J. / Jiang, H. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 127
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GT2010-22288 Heat Transfer Characteristics of an Oblique Jet Impingement Configuration in a Passage With Ribbed SurfacesHoefler, F. / Naik, S. / Schueren, S. / von Wolfersdorf, J. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 139
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GT2010-22362 Investigation of Sand Particle Deposition and Erosion Within a Short Pin Fin ArrayCowan, J.B. / Tafti, D.K. / Kohli, A. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 151
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GT2010-22376 Simulations of Multi-Phase Particle Deposition on Endwall Film-CoolingLawson, S.A. / Thole, K.A. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 163
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GT2010-22407 Numerical Investigation of Heat Transfer and Flow Characteristics in a Steam-Cooled Square Ribbed DuctShui, L. / Gao, J. / Xu, L. / Wang, X. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 173
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GT2010-22432 Experimental Investigation of Conjugate Heat Transfer in a Rib-Roughened Trailing Edge Channel With Crossing-JetsColetti, F. / Scialanga, M. / Arts, T. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 185
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GT2010-22442 Comparisons of Flow Friction and Heat Transfer Performance in Rectangular Channels With Pin Fin-Dimple, Pin Fin and Dimple ArraysRao, Y. / Wan, C. / Zang, S. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 197
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GT2010-22562 A Simplified Approach to Design Transverse Ribs Which Array Alternately in Rectangular ChannelZhang, H. / Wang, J. / Wu, X. / Lu, H. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 205
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GT2010-22563 Numerical Investigations of Fluid Flow and Heat Transfer Performances of Semiattached Rib Channel DesignWang, J. / Liu, H. / Mao, M. / Li, X. / Zhang, Z. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 213
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GT2010-22572 Computational and Experimental Study of Conjugate Heat Transfer From a Flat Plate With an Impinging JetPanda, R.K. / Prasad, B.V.S.S.S. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 223
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GT2010-22609 Heat Transfer in a Rotating Rectangular Channel With Two Opposite Walls Roughened With Spherical Protrusions at High Rotation NumbersChang, S.W. / Liou, T.-M. / Chen, W.C. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 233
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GT2010-22636 Numerical Validation of Heat Transfer Augmentation Factor in Serpentine Passages With Ribbed WallsRamakumar, B.V.N. / Kollati, V.R. / Liu, J.S. / Crites, D.C. / Goswami, S. / Kulkarni, V. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 245
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GT2010-22657 Investigation of Coriolis Forces Effect of Flow Structure and Heat Transfer Distribution in a Rotating Dimpled ChannelElyyan, M.A. / Tafti, D.K. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 255
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GT2010-22700 Effect of Temperature Nonuniformity on Heat Transfer in an Unshrouded Transonic HP Turbine: An Experimental and Computational InvestigationQureshi, I. / Smith, A.D. / Chana, K.S. / Povey, T. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 271
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GT2010-22713 Heat Transfer for the Blade of a Cooled Stage and One-Half High-Pressure Turbine: Part I - Influence of Cooling VariationMathison, R.M. / Haldeman, C.W. / Dunn, M.G. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 285
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GT2010-22715 Heat Transfer for the Blade of a Cooled Stage and One-Half High-Pressure Turbine: Part II - Independent Influences of Vane Trailing Edge and Purge CoolingMathison, R.M. / Haldeman, C.W. / Dunn, M.G. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 299
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GT2010-22716 Aerodynamics and Heat Transfer for a Cooled One and One-Half Stage High-Pressure Turbine: Part I - Vane Inlet Temperature Profile Generation and MigrationMathison, R.M. / Haldeman, C.W. / Dunn, M.G. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 313
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GT2010-22718 Aerodynamics and Heat Transfer for a Cooled One and One-Half Stage High-Pressure Turbine: Part II-Influence of Inlet Temperature Profile on Blade Row and ShroudMathison, R.M. / Haldeman, C.W. / Dunn, M.G. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 323
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GT2010-22720 Heat Transfer Investigations in Multiple Impinging Jets at Low Reynolds NumberRao, A.G. / Kitron-Belinkov, M. / Krapp, V. / Levy, Y. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 335
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GT2010-22779 Transonic Turbine Blade Tip Aero-Thermal Performance With Different Tip Gaps: Part I - Tip Heat TransferZhang, Q. / O Dowd, D.O. / He, L. / Oldfield, M.L.G. / Ligrani, P.M. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 347
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GT2010-22780 Transonic Turbine Blade Tip Aero-Thermal Performance With Different Tip Gaps: Part II - Tip Aerodynamic LossO Dowd, D.O. / Zhang, Q. / Usandizaga, I. / He, L. / Ligrani, P.M. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 357
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GT2010-22794 Aero-Thermal Performance of a Winglet at Engine Representative Mach and Reynolds NumbersO Dowd, D.O. / Zhang, Q. / He, L. / Oldfield, M.L.G. / Ligrani, P.M. / Cheong, B.C.Y. / Tibbott, I. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 369
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GT2010-22832 Heat Transfer in Trailing Edge Wedge-Shaped Pin-Fin Channels With Slot Ejection Under High Rotation NumbersRallabandi, A.P. / Liu, Y.-H. / Han, J.-C. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 381
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GT2010-22870 Numerical Predictions of the Effect of Rotation on Fluid Flow and Heat Transfer in an Engine-Similar Two-Pass Internal Cooling Channel With Smooth and Ribbed WallsSchuler, M. / Dreher, H.-M. / Elfert, M. / Neumann, S.O. / Weigand, B. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 395
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GT2010-22956 High Temperature Turbine First Stage Vane Wake to Stator Heat Shield Interaction on Outer CasingCochet, M. / Arzel, T. / Gritsch, M. / Stephan, B. / Schnieder, M. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 405
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GT2010-22975 A Transient Inrfrared Technique for Measuring Surface and Endwall Heat Transfer in a Transonic Turbine CascadeReagle, C. / Newman, A. / Xue, S. / Ng, W. / Ekkad, S. / Moon, H.K. / Zhang, L. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 413
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GT2010-22976 Micro Channels With Manufacturing Roughness LevelsWeaver, S.A. / Barringer, M.D. / Thole, K.A. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 423
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GT2010-22979 Geometrical Uncertainty and Film Cooling: Fillet RadiiMontomoli, F. / Massini, M. / Salvadori, S. / Martelli, F. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 433
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GT2010-22987 Temperature Predictions and Comparison With Measurements for the Blade Leading Edge and Platform of a 1-1/2 Stage Transonic HP TurbineMathison, R.M. / Wishart, M.B. / Haldeman, C.W. / Dunn, M.G. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 447
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GT2010-23004 Experimental Measurements and Computational Predictions for an Internally Cooled Simulated Turbine Vane With 90 Degree Rib TurbulatorsDees, J.E. / Bogard, D.G. / Ledezma, G.A. / Laskowski, G.M. / Tolpadi, A.K. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 457
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GT2010-23008 Momentum and Thermal Boundary Layer Development on an Internally Cooled Turbine VaneDees, J.E. / Bogard, D.G. / Ledezma, G.A. / Laskowski, G.M. / Tolpadi, A.K. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 471
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GT2010-23031 Study of Flow Through a Stationary Ribbed Channel for Blade CoolingAmano, R. / Guntur, K. / Lucci, J.M. / Ashitaka, Y. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 479
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GT2010-23076 Experimental Flow Visualizations Study in a Trapezoidal Duct With Impingement Jets and Cross Flow Near the Leading EdgeLiu, H. / Liu, S. / Qiang, H. / Liu, C. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 491
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GT2010-23227 Effects of Pin Detached Space on Heat Transfer and From Pin Fin ArraysSiw, S.C. / Chyu, M.K. / Shih, T.I.-P. / Alvin, M.A. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 501
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GT2010-23247 Conjugate Heat Transfer Analysis of a High Pressure Air-Cooled Gas Turbine VaneWang, Z. / Yan, P. / Huang, H. / Han, W. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 509
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GT2010-23251 Conjugate Heat Transfer Numerical Validation and PSE Analysis of Transonic Internally-Cooled Turbine CascadeYan, P. / Wang, Z. / Han, W. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 517
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GT2010-23314 Prediction of the Influence of Upstream Wake Passing on Downstream Blade Row External Heat Transfer Coefficient: A New Physically-Based MethodChana, K.S. / Haller, B.R. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 525
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GT2010-23445 Fully-Cooled Single Stage HP Transonic Turbine: Part II - Influence of Cooling Mass Flow Changes and Inlet Temperature Profiles on Blade and Shroud Heat-TransferHaldeman, C.W. / Dunn, M.G. / Mathison, R.M. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 539
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GT2010-23446 Fully-Cooled Single Stage HP Transonic Turbine: Part I - Influence of Cooling Mass Flow Variations and Inlet Temperature Profiles on Blade Internal and External AerodynamicsHaldeman, C.W. / Dunn, M.G. / Mathison, R.M. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 555
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GT2010-23510 PIV-Measurement of Secondary Flow in a Rotating Two-Pass Cooling System With an Improved Sequencer TechniqueElfert, M. / Schroll, M. / Forster, W. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 569
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GT2010-23511 Aerothermal Research for Turbine Components: An Overview of the European AITEB-2 ProjectJanke, E. / Wolf, T. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 579
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GT2010-23521 Experimental and Numerical Cross-Over Jet Impingement in an Airfoil Trailing-Edge Cooling ChannelTaslim, M.E. / Nongsaeng, A. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 593
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GT2010-23536 Numerical and Experimental Investigation of Turning Flow Effects of Innovative Pin Fin Arrangements for Trailing Edge Cooling ConfigurationsBianchini, C. / Facchini, B. / Simonetti, F. / Tarchi, L. / Zecchi, S. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 605
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GT2010-23653 Heat Transfer Investigation of an Aggressive Intermediate Turbine Duct: Part 1 - Experimental InvestigationOsso, C.A. / Johansson, T.G. / Wallin, F. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 615
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GT2010-23655 Composition Dependent Model for the Prediction of Syngas Ash Deposition With Application to a Leading Edge Turbine VaneSreedharan, S.S. / Tafti, D.K. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 627
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GT2010-23660 Effects of Thermal Radiation on Air Plasma Spray (APS) Coated Gas Turbine BladeAkwaboa, S. / Mensah, P. / Diwan, R. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 635
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GT2010-23679 Internal Cooling Using Novel Swirl Enhancement Strategies in a Slot Shaped Single Pass ChannelSegura, D. / Acharya, S. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 645
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GT2010-23694 Analysis of Unsteady Tip and Endwall Heat Transfer in a Highly Loaded Transonic Turbine StageShyam, V. / Ameri, A. / Chen, J.-P. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 657
-
GT2010-23711 Numerical Study of Flow and Heat Transfer of Impingement Cooling on Model of Turbine Blade Leading EdgeLiu, Z. / Feng, Z. / Song, L. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 675
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GT2010-23757 Channel Height and Jet Spacing Effect on Heat Transfer and Uniformity Coefficient on an Inline Row Impingement ChannelRicklick, M. / Claretti, R. / Kapat, J.S. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 685
-
GT2010-23800 Experimental Study of Surface Roughness Effects on a Turbine Airfoil in a Linear Cascade: Part I - External Heat TransferLorenz, M. / Schulz, A. / Bauer, H.-J. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 699
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GT2010-23801 Experimental Study of Surface Roughness Effects on a Turbine Airfoil in a Linear Cascade: Part II - Aerodynamic LossesLorenz, M. / Schulz, A. / Bauer, H.-J. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 713
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GT2010-23855 Aerodynamics and Heat Transfer for a Cooled One and One-Half Stage High-Pressure Turbine: Part III - Impact of Hot Streak Characteristics on Blade Row Heat FluxMathison, R.M. / Haldeman, C.W. / Dunn, M.G. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 725
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GT2010-22702 Effect of Simulated Combustor Temperature Nonuniformity on HP Vane and Endwall Heat Transfer: An Experimental and Computational InvestigationQureshi, I. / Beretta, A. / Povey, T. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 743
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GT2010-22855 Deposition in a Turbine Cascade With Combusting FlowSmith, C. / Barker, B. / Clum, C. / Bons, J. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 753
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GT2010-22936 Combined Effect of Slot Injection, Effusion Array and Dilution Hole on the Heat Transfer Coefficient of a Real Combustor Liner: Part 1 - Experimental AnalysisFacchini, B. / Coutandin, D. / Maiuolo, F. / Tarchi, L. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 763
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GT2010-22937 Combined Effect of Slot Injection, Effusion Array and Dilution Hole on the Heat Transfer Coefficient of a Real Combustor Liner: Part 2 - Numerical AnalysisAndreini, A. / Ceccherini, A. / Facchini, B. / Coutandin, D. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 773
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GT2010-22942 Numerical Study of Aerodynamic Losses of Effusion Cooling Holes in Aero-Engine Combustor LinersAndreini, A. / Bonini, A. / Caciolli, G. / Facchini, B. / Taddei, S. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 787
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GT2010-22986 Study of Flow and Convective Heat Transfer in a Simulated Scaled Up Low Emission Annular CombustorSedalor, T. / Patil, S. / Ekkad, S. / Tafti, D. / Kim, Y. / Moon, H.-K. / Srinivasan, R. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 795
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GT2010-23082 The Effect of Geometry on the Aerodynamics of a Prototype Gas Turbine CombustorMohammad, B. / Jeng, S.-M. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 809
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GT2010-23083 Influence of the Primary Jets and Fuel Injection on the Aerodynamics of a Prototype Annular Gas Turbine Combustor SectorMohammad, B. / Jeng, S.-M. / Andac, M.G. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 825
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GT2010-23197 Heat Transfer and Pressure Losses of W-Shaped Small Ribs at High Reynolds Numbers for Combustor LinerHagari, T. / Ishida, K. / Oda, T. / Douura, Y. / Kinoshita, Y. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 835
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GT2010-23234 Heat Transfer and Pressure Drop in Combustor Cooling Channels With Combinations of Geometrical ElementsKunstmann, S. / von Wolfersdorf, J. / Ruedel, U. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 847
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GT2010-23556 Hot Streak Migration in a Turbine Stage: Integrated Design to Improve Aero-Thermal PerformanceBasol, A.M. / Jenny, P. / Ibrahim, M. / Kalfas, A. / Abhari, R.S. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 861
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GT2010-23664 The Effects of Localized Blade Endwall Suction on Secondary Flows and Heat TransferHollis, R. / Bons, J.P. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 873
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GT2010-22694 Experimental Heat Transfer Investigation in a Multisplitter LP Vane ArchitecturePinilla, V. / Solano, J.P. / Paniagua, G. / Lavagnoli, S. / Yasa, T. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 883
-
GT2010-22903 Sensitivity of Numerical Simulations of Low-Reynolds Number Flow Over the T106 Turbine Bladede Saint Victor, X. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 891
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GT2010-23275 Calculation of Steady and Periodic Unsteady Blade Surface Heat Transfer in Separated Transitional FlowPacciani, R. / Rubechini, F. / Arnone, A. / Lutum, E. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 901
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GT2010-23331 Modeling Separation: Induced Transition Using a Non-Linear Three Equation Turbulence Model and a Reynolds Stress Turbulence ModelVlahostergios, Z. / Yakinthos, K. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 913
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GT2010-22025 Numerical Analysis of Heat Transfer and Flow Stability in an Open Rotating Cavity Using the Maximum Entropy Production PrincipleBohn, D. / Krewinkel, R. / Wolff, A. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 921
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GT2010-22069 Influence of Honeycomb Facings on the Temperature Distribution in Labyrinth SealsWeinberger, T. / Dullenkopf, K. / Bauer, H.-J. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 931
-
GT2010-22071 A Probabilistic Secondary Flow System Design Process for Gas Turbine EnginesMirzaMoghadam, A.V. / Ramerth, D.L. / Kiratsingh, A. / Banda, G. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 943
-
GT2010-22130 Heat Transfer in Turbine Hub Cavities Adjacent to the Main Gas PathDixon, J.A. / Guijarro, A. / Bauknecht, A. / Coren, D. / Atkins, N. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 955
-
GT2010-22203 1D Tool for Stator-Rotor Cavities Integrated Into a Fluid Network Solver of Heavy-Duty Gas Turbine Secondary Air SystemBonzani, F. / Bozzi, L. / Mantero, M. / Vinci, A. / Innocenti, L. / Micio, M. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 965
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GT2010-22311 Aerothermal Impact of the Interaction Between Hub Leakage and Mainstream Flows in Highly-Loaded HP Turbine BladesPopovic, I. / Hodson, H.P. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 977
-
GT2010-22434 Parametric Single Gap Turbine Rim Seal Model With Boundary Generation for Asymmetric External FlowHuning, M. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 991
-
GT2010-22544 Local Measurements of Disc Heat Transfer in Heated Rotating Cavities for Several Flow RegimesGunther, A. / Odenbach, S. / Uffrecht, W. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 1001
-
GT2010-22593 The Deduction of the Integral and the Estimation of the Local Core Rotation Ratio by Telemetric Pressure Measurements in a Two Cavity Test RigUffrecht, W. / Gunther, A. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 1013
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GT2010-22661 Modelling the Labyrinth Seal Discharge Coefficient Using Data Mining MethodsPychynski, T. / Mikut, R. / Dullenkopf, K. / Bauer, H.-J. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 1025
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GT2010-22673 Coupled Aero-Thermo-Mechanical Simulation for a Turbine Disc Through a Full Transient CycleSun, Z. / Chew, J.W. / Hills, N.J. / Lewis, L. / Mabilat, C. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 1037
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GT2010-22684 Thermo Mechanical FEA/CFD Coupling of an Interstage Seal Cavity Using Torsional Spring AnalogyAmirante, D. / Hills, N.J. / Barnes, C.J. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 1051
-
GT2010-22691 Experimental Study of Discharge Coefficients for Radial Orifices in High-Speed Rotating ShaftsSousek, J. / Pfitzner, M. / Niehuis, R. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 1061
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GT2010-22710 CFD-FE Automation and Thermo-Fluid Characterisation of an IP Turbine CavityBagshaw, D. / Alizadeh, S. / Mabilat, C. / Lewis, L. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 1071
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GT2010-22729 Simulations of Flow Ingestion and Related Structures in a Turbine Disk CavityJulien, S. / Lefrancois, J. / Dumas, G. / Caron, J.-F. / Marini, R. / Boutet-Blais, G. / Lapointe, S. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 1081
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GT2010-22743 Numerical Investigation of Leakage and Power Loss for Different Seal Types in Turbine Stage EnvironmentYang, R. / Yang, J. / Qi, M. / Shi, L. / Peng, Z. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 1091
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GT2010-22775 Investigation of Augmented Angel Wing Sealing Through the Use of Surface Concavity ArraysBunker, R.S. / Sheng, N. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 1103
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GT2010-22813 Transient Thermodynamic, Thermal and Structure Analysis of a Steam Turbine During its Start-UpRzadkowski, R. / Lampart, P. / Kwapisz, L. / Szymaniak, M. / Drewczynski, M. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 1113
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GT2010-22824 Response of a Disk Cavity Flow to Gas Turbine Engine TransientsMay, D. / Chew, J.W. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 1123
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GT2010-22838 Calculation of Disk Temperatures in Gas Turbine Rotor-Stator Cavities Using Conjugate Heat TransferVadvadgi, A.S. / Yavuzkurt, S. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 1133
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GT2010-22877 Effects of Clearances on the Leakage Flow Characteristics of Two Kinds of Brush Seals and Referenced Labyrinth SealLi, J. / Huang, Y. / Li, Z. / Feng, Z. / Yang, H. / Yang, J. / Shi, L. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 1143
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GT2010-22935 An Efficient Procedure for the Analysis of Heavy Duty Gas Turbine Secondary Flows in Different Operating ConditionsCerutti, M. / Bozzi, L. / Carcasci, C. / Bonzani, F. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 1155
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GT2010-22962 Large-Eddy Simulation of Rim Seal IngestionO Mahoney, T.S.D. / Scanlon, T. / Hills, N.J. / Chew, J.W. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 1167
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GT2010-22964 CFD Analysis of Flow and Heat Transfer in a Direct Transfer Pre-Swirl SystemJaviya, U. / Chew, J. / Hills, N. / Zhou, L. / Wilson, M. / Lock, G. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 1179
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GT2010-23194 Study on the Leakage and Deformation Characteristics of the Finger Seals by Using Numerical SimulationZhang, H. / Zheng, Q. / Yue, G. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 1191
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GT2010-23256 Aerodynamic Performance of Stepped Labyrinth Seals for Gas Turbine ApplicationsKang, Y. / Kim, T.S. / Kang, S.Y. / Moon, H.K. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 1201
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GT2010-23294 CFD Modelling and LDA Measurements for the Air-Flow in an Aero-Engine Front Bearing ChamberAidarinis, J. / Missirlis, D. / Yakinthos, K. / Goulas, A. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 1209
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GT2010-23312 Direct Outer Ring Cooling of a High Speed Jet Engine Mainshaft Ball Bearing: Experimental Investigation ResultsGloeckner, P. / Dullenkopf, K. / Flouros, M. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 1217
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GT2010-23346 Prediction of Ingress Through Turbine Rim Seals: Part 1 - Externally-Induced IngressOwen, J.M. / Zhou, K. / Wilson, M. / Pountney, O. / Lock, G. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 1235
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GT2010-23349 Prediction of Ingress Through Turbine Rim Seals: Part 2 - Combined IngressOwen, J.M. / Pountney, O. / Lock, G. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 1247
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GT2010-23392 Impacts of Engine Secondary Air System Uncertainties on Gas Turbine Compressor Heat TransferAlizadeh, S. / Gopinathrao, N. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 1259
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GT2010-23450 An Advanced Multi-Configuration Stator Well Cooling Test FacilityCoren, D.D. / Atkins, N.R. / Turner, J.R. / Eastwood, D.E. / Davies, S. / Childs, P.R.N. / Dixon, J. / Scanlon, T.S. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 1271
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GT2010-23469 Labyrinth Seal Technology Within the Dutch Aero Engine ClusterKool, G.A. / Kloosterman, A. / Soemarwoto, B. / Versluis, J. / Janssen, R. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 1283
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GT2010-23532 CFD Methods for Shear Driven Liquid Wall FilmsHashmi, A.A. / Dullenkopf, K. / Koch, R. / Bauer, H.-J. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 1293
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GT2010-23629 Film Riding Leaf Seals for Improved Shaft SealingGrondahl, C.M. / Dudley, J.C. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 1301
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GT2010-22060 A Parametric Study on the Effect of Sister Hole Location on Active Film Cooling Flow ControlEly, M.J. / Jubran, B.A. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 1313
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GT2010-22077 A Preliminary Numerical Study on the Effect of High Freestream Turbulence on Anti-Vortex Film Cooling Design at High Blowing RatioHunley, B.K. / Nix, A.C. / Heidmann, J.D. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 1323
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GT2010-22117 Effects of Trenched Holes on Film Cooling of a Contoured Endwall Nozzle VaneBarigozzi, G. / Franchini, G. / Perdichizzi, A. / Ravelli, S. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 1335
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GT2010-22120 Sensitivity Analysis for Film Effectiveness on a Round Film Hole Embedded in a Trench Using Conjugate Heat Transfer Numerical ModelNguyen, C.Q. / Tran, N.V.T. / Bernier, B.C. / Ho, S.H. / Kapat, J.S. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 1347
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GT2010-22188 Block-Spectral Approach to Film-Cooling ModellingHe, L. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 1359
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GT2010-22237 Film Cooling Performance of Waist-Shaped Slot HolesLiu, C.-l. / Zhu, H.-r. / Bai, J.-t. / Xu, D.-c. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 1371
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GT2010-22308 CFD Predictions of Single Row Film Cooling With Inclined Holes: Influence of Hole Outlet GeometryOguntade, H.I. / Andrews, G.E. / Burns, A. / Ingham, D. / Pourkashanian, M. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 1387
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GT2010-22325 Assessment of URANS and DES for Prediction of Leading Edge Film CoolingTakahashi, T. / Funazaki, K.-i. / Salleh, H.B. / Sakai, E. / Watanabe, K. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 1401
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GT2010-22327 Estimating the Loss Associated With Film Cooling for a Turbine StageLim, C.H. / Pullan, G. / Northall, J. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 1415
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GT2010-22337 Film Cooling Performance of the Embedded Holes in Trenches With Compound AnglesLi, J. / Ren, J. / Jiang, H. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 1425
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GT2010-22358 Velocity Measurements Around Film Cooling Holes With DepositionHaase, K. / Bons, J.P. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 1437
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GT2010-22382 Influence of Different Shoulder Widths on Film Cooling Characteristics on GE-E3 Blade TipWang, J. / Zhang, D.H. / Zeng, M. / Wang, Q.W. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 1447
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GT2010-22398 Shape Optimization of a Laidback Fan-Shaped Film-Cooling Hole to Enhance Cooling PerformanceLee, K.-D. / Kim, K.-Y. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 1459
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GT2010-22411 Particle-Image Velocimetry Measurements of Film Cooling in an Adverse Pressure Gradient FlowJessen, W. / Konopka, M. / Schroder, W. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 1471
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GT2010-22475 Aerodynamic Comparison and Validation of RANS, URANS and SAS Simulations of Flat Plate Film-CoolingVoigt, S. / Noll, B. / Aigner, M. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 1481
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GT2010-22559 Computational Investigations on Leading Edge Film Cooling of AGTB Blade With Cylindrical and Trenched Compound Angle HolesZhang, D.H. / Zeng, M. / Wang, Q.W. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 1491
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GT2010-22603 Experimental Investigation Into Unsteady Effects on Film CoolingFawcett, R.J. / Wheeler, A.P.S. / He, L. / Taylor, R. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 1503
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GT2010-22604 Film Cooling Effectiveness Comparison Between Shaped- and Double Jet Film Cooling Holes in a Row ArrangementKusterer, K. / Elyas, A. / Bohn, D. / Sugimoto, T. / Tanaka, R. / Kazari, M. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 1517
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GT2010-22774 Enhanced Film Cooling Effectiveness With New Shaped HolesLiu, J.S. / Malak, M.F. / Ramachandran, D. / Tapia, L.A. / Srinivasan, B. / Crites, D.C. / Muthiah, G. / Venkataramanan, J. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 1529
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GT2010-22781 Influence of Coolant Density on Turbine Blade Film-Cooling Using Pressure Sensitive Paint TechniqueNarzary, D.P. / Liu, K.-C. / Rallabandi, A.P. / Han, J.-C. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 1541
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GT2010-22787 A Model for Cylindrical Hole Film Cooling: Part I - A Correlation for Jet-Flow With Application to Film CoolingKampe, T.a.d. / Zehe, F. / Volker, S. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 1551
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GT2010-22788 A Model for Cylindrical Hole Film Cooling: Part II - Model Formulation, Implementation and ResultsKampe, T.a.d. / Volker, S. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 1561
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GT2010-22808 Heat Transfer Performance of Fan-Shaped Film Cooling Holes: Part I - Experimental AnalysisBonanni, L. / Facchini, B. / Tarchi, L. / Maritano, M. / Traverso, S. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 1573
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GT2010-22809 Heat Transfer Performance of Fan-Shaped Film Cooling Holes: Part II - Numerical AnalysisBianchini, C. / Facchini, B. / Mangani, L. / Maritano, M. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 1585
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GT2010-22931 Endwall Effusion Cooling System Behaviour Within a High-Pressure Turbine Cascade: Part 1 - Aerodynamic MeasurementsSacchi, M. / Simoni, D. / Ubaldi, M. / Zunino, P. / Zecchi, S. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 1595
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GT2010-22932 Endwall Effusion Cooling System Behaviour Within a High-Pressure Turbine Cascade: Part 2 - Heat Transfer and Effectiveness MeasurementsFacchini, B. / Tarchi, L. / Toni, L. / Zecchi, S. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 1607
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GT2010-22958 Film Cooling Calculations With an Iterative Conjugate Heat Transfer Approach Using Empirical Heat Transfer Coefficient CorrectionsDhiman, S. / Yavuzkurt, S. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 1617
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GT2010-22968 Effects of an Axisymmetric Contoured Endwall on a Nozzle Guide Vane: Adiabatic Effectiveness MeasurementsThrift, A.A. / Thole, K.A. / Hada, S. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 1629
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GT2010-22970 Effects of an Axisymmetric Contoured Endwall on a Nozzle Guide Vane:Convective Heat Transfer MeasurementsThrift, A.A. / Thole, K.A. / Hada, S. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 1641
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GT2010-22984 Computational Predictions of Heat Transfer and Film-Cooling for a Turbine Blade With Non-Axisymmetric Endwall ContouringLynch, S.P. / Kohli, A. / Thole, K.A. / Lehane, C. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 1655
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GT2010-23002 Evaluating the Effects of Internal Impingement Cooling on a Film Cooled Turbine Blade Leading EdgeRavelli, S. / Dobrowolski, L. / Bogard, D.G. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 1667
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GT2010-23030 The Experimental and Numerical Research for Linear Cascade Film Cooling With Different Hole ShapesLu, Y. / Hong, Y. / Lin, Z. / Yuan, X. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 1677
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GT2010-23032 Influence of Flow Structure on Shaped Hole Film Cooling PerformanceLaveau, B. / Abhari, R.S. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 1691
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GT2010-23053 Effect of Density Ratio on Flat Plate Film Cooling With Shaped Holes Using PSPWright, L.M. / McClain, S.T. / Clemenson, M.D. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 1703
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GT2010-23054 Effect of Freestream Turbulence Intensity on Film Cooling Jet Structure and Surface Effectiveness Using PIV and PSPWright, L.M. / McClain, S.T. / Clemenson, M.D. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 1719
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GT2010-23090 Film Cooling Performance of Sharp-Edged Diffusor Holes With Lateral InclinationHeneka, C. / Schulz, A. / Heselhaus, A. / Crawford, M. / Bauer, H.-J. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 1729
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GT2010-23178 Film Cooling Effect of Rotor-Stator Purge Flow on Endwall Heat/Mass TransferPapa, M. / Srinivasan, V. / Goldstein, R.J. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 1739
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GT2010-23179 Flow Visualization Study of Passive Flow Control Features on a Film-Cooled Turbine Blade Leading EdgeCarroll, D.R. / King, P.I. / Rutledge, J.L. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 1751
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GT2010-23203 Heat Transfer and Effectiveness on the Film Cooled Tip and Inner Rim Surfaces of a Turbine BladePark, J.S. / Lee, D.H. / Rhee, D.-H. / Cho, H.H. / Kang, S.-H. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 1763
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GT2010-23288 Heat Transfer and Film Cooling of Blade Tips and EndwallsNaik, S. / Georgakis, C. / Hofer, T. / Lengani, D. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 1777
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GT2010-23308 Fan Shaped and Cylindrical Holes Studied in Vane Film Cooling Test RigKinell, M. / Utriainen, E. / Hylen, J. / Gustavsson, J. / Bradley, A. / Karlsson, M. / Wren, J. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 1785
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GT2010-23321 Effect of Vane/Blade Relative Positions and Showerhead Film Cooling on a Stationary Blade: Heat TransferLee, D.H. / Rhee, D.-H. / Kim, K.M. / Cho, H.H. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 1795
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GT2010-23438 Accuracy of Conventional Adiabatic Effectiveness and Heat Transfer Augmentation Factors in Predicting Heat Flux Into a Turbine Blade Leading EdgeDobrowolski, L.D. / Bogard, D.G. / Ravelli, S. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 1805
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GT2010-23458 Conjugate Heat Transfer Analysis of NASA C3X Film Cooled Vane With an Object-Oriented CFD CodeMangani, L. / Cerutti, M. / Maritano, M. / Spel, M. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 1815
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GT2010-23543 Aerothermodynamics of a High-Pressure Turbine Blade With Very High Loading and Vortex GeneratorsGomes, R.A. / Niehuis, R. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 1829
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GT2010-23578 Trailing Edge Film Cooling of Gas Turbine Airfoils: External Cooling Performance of Various Internal Pin Fin ConfigurationsHorbach, T. / Schulz, A. / Bauer, H.-J. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 1841
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GT2010-23597 A Correlation Approach to Predicting Film Cooled Turbine Vane Heat TransferBoyle, R.J. / Ameri, A.A. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 1857
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GT2010-23680 The Role of Density Ratio and Blowing Ratio on Film Cooling in a Vane PassagePost, J.W. / Acharya, S. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 1869
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GT2010-23688 Squealer Tip Heat Transfer With Film CoolingAcharya, S. / Kramer, G. / Moreaux, L. / Nakamata, C. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 1879
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GT2010-23707 Overall Effectiveness for a Film Cooled Turbine Blade Leading Edge With Varying Hole PitchDyson, T.E. / Bogard, D.G. / Piggush, J.D. / Kohli, A. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 1889
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GT2010-23725 Total Cooling Effectiveness on a Staggered Full-Coverage Film Cooling Plate With Impinging JetJung, E.Y. / Lee, D.H. / Oh, S.H. / Kim, K.M. / Cho, H.H. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 1897
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GT2010-23732 Comparison of Film Effectiveness and Cooling Uniformity of Conical and Cylindrical-Shaped Film Hole With Coolant-Exit Temperature CorrectionNguyen, C.Q. / Johnson, P.L. / Bernier, B.C. / Ho, S.H. / Kapat, J.S. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010