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Volume 133, Issue 1
January 2011
Issue Cover
ISSN 0889-504X
EISSN 1528-8900
In this Issue

Research Papers

Heat Transfer From Low Aspect Ratio Pin Fins
Michael E. Lyall, Alan A. Thrift, Karen A. Thole, Atul Kohli
J. Turbomach. January 2011, 133(1): 011001. doi: https://doi.org/10.1115/1.2812951
View articletitled, Heat Transfer From Low Aspect Ratio Pin Fins
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Topics: Fins , Heat transfer , Reynolds number
A Film-Cooling Correlation for Shaped Holes on a Flat-Plate Surface
Will F. Colban, Karen A. Thole, David Bogard
J. Turbomach. January 2011, 133(1): 011002. doi: https://doi.org/10.1115/1.4002064
View articletitled, A Film-Cooling Correlation for Shaped Holes on a Flat-Plate Surface
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Topics: Coolants , Cooling , Film cooling , Flat plates , Turbulence , Gas turbines , Flow (Dynamics)
Development of a Two-Dimensional Streamline Curvature Code
Ioannis Templalexis, Pericles Pilidis, Vassilios Pachidis, Petros Kotsiopoulos
J. Turbomach. January 2011, 133(1): 011003. doi: https://doi.org/10.1115/1.2720877
View articletitled, Development of a Two-Dimensional Streamline Curvature Code
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Topics: Blades , Compressors , Computer software , Design , Flow (Dynamics) , Students , Supersonic flow , Pressure
Investigation of Periodically Unsteady Flow in a Radial Pump by CFD Simulations and LDV Measurements
Jianjun Feng, Friedrich-Karl Benra, Hans Josef Dohmen
J. Turbomach. January 2011, 133(1): 011004. doi: https://doi.org/10.1115/1.4000486
View articletitled, Investigation of Periodically Unsteady Flow in a Radial Pump by CFD Simulations and LDV Measurements
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Topics: Blades , Computational fluid dynamics , Diffusers , Flow (Dynamics) , Impellers , Pumps , Simulation , Turbulence , Unsteady flow , Design
Experimental Measurements of Gas Turbine Flow Capacity Using a Novel Transient Technique
T. Povey, M. Sharpe, A. Rawlinson
J. Turbomach. January 2011, 133(1): 011005. doi: https://doi.org/10.1115/1.4000481
View articletitled, Experimental Measurements of Gas Turbine Flow Capacity Using a Novel Transient Technique
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Topics: Flow (Dynamics) , Pressure , Uncertainty , Nozzle guide vanes , Transients (Dynamics) , Venturi tubes , Nozzles
Numerical Assessment of the Noise Signature Sidewall Contamination of a Linear Cascade With Moving Bars
Manuel A. Burgos, Roque Corral
J. Turbomach. January 2011, 133(1): 011006. doi: https://doi.org/10.1115/1.4000487
View articletitled, Numerical Assessment of the Noise Signature Sidewall Contamination of a Linear Cascade With Moving Bars
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Topics: Airfoils , Cascades (Fluid dynamics) , Flow (Dynamics) , Pressure
Investigation of Blade Tip Interaction With Casing Treatment in a Transonic Compressor—Part I: Particle Image Velocimetry
M. Voges, R. Schnell, C. Willert, R. Mönig, M. W. Müller, C. Zscherp
J. Turbomach. January 2011, 133(1): 011007. doi: https://doi.org/10.1115/1.4000489
View articletitled, Investigation of Blade Tip Interaction With Casing Treatment in a Transonic Compressor—Part I: Particle Image Velocimetry
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Topics: Blades , Compressors , Flow (Dynamics) , Particulate matter , Rotors , Computational fluid dynamics , Lasers
Investigation of Blade Tip Interaction With Casing Treatment in a Transonic Compressor—Part II: Numerical Results
R. Schnell, M. Voges, R. Mönig, M. W. Müller, C. Zscherp
J. Turbomach. January 2011, 133(1): 011008. doi: https://doi.org/10.1115/1.4000490
View articletitled, Investigation of Blade Tip Interaction With Casing Treatment in a Transonic Compressor—Part II: Numerical Results
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Topics: Blades , Compressors , Flow (Dynamics) , Rotors , Boundary-value problems , Pressure , Simulation , Stators
Redesign of a Low Speed Turbine Stage Using a New Viscous Inverse Design Method
Benedikt Roidl, Wahid Ghaly
J. Turbomach. January 2011, 133(1): 011009. doi: https://doi.org/10.1115/1.4000491
View articletitled, Redesign of a Low Speed Turbine Stage Using a New Viscous Inverse Design Method
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Topics: Blades , Design , Design methodology , Flow (Dynamics) , Pressure , Rotors , Stators , Turbines , Geometry
Effects of Syngas Ash Particle Size on Deposition and Erosion of a Film Cooled Leading Edge
Ali Rozati, Danesh K. Tafti, Sai Shrinivas Sreedharan
J. Turbomach. January 2011, 133(1): 011010. doi: https://doi.org/10.1115/1.4000492
View articletitled, Effects of Syngas Ash Particle Size on Deposition and Erosion of a Film Cooled Leading Edge
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Topics: Coolants , Erosion , Particulate matter , Flow (Dynamics) , Particle size , Blades , Temperature , Syngas
An Integrated System for the Aerodynamic Design of Compression Systems—Part I: Development
Tiziano Ghisu, Geoffrey T. Parks, Jerome P. Jarrett, P. John Clarkson
J. Turbomach. January 2011, 133(1): 011011. doi: https://doi.org/10.1115/1.4000534
View articletitled, An Integrated System for the Aerodynamic Design of Compression Systems—Part I: Development
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Topics: Design , Optimization , Gas turbines
An Integrated System for the Aerodynamic Design of Compression Systems—Part II: Application
Tiziano Ghisu, Geoffrey T. Parks, Jerome P. Jarrett, P. John Clarkson
J. Turbomach. January 2011, 133(1): 011012. doi: https://doi.org/10.1115/1.4000535
View articletitled, An Integrated System for the Aerodynamic Design of Compression Systems—Part II: Application
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Topics: Compression , Design , Optimization , Compressors , Ducts , Gas turbines
The Influence of Blade Lean on Straight and Annular Turbine Cascade Flow Field
Gabriele D’Ippolito, Vincenzo Dossena, Alessandro Mora
J. Turbomach. January 2011, 133(1): 011013. doi: https://doi.org/10.1115/1.4000536
View articletitled, The Influence of Blade Lean on Straight and Annular Turbine Cascade Flow Field
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Topics: Blades , Flow (Dynamics) , Pressure , Cascades (Fluid dynamics) , Pressure gradient , Flow visualization , Vorticity
Experimental Simulation of a Film Cooled Turbine Blade Leading Edge Including Thermal Barrier Coating Effects
Jonathan Maikell, David Bogard, Justin Piggush, Atul Kohli
J. Turbomach. January 2011, 133(1): 011014. doi: https://doi.org/10.1115/1.4000537
View articletitled, Experimental Simulation of a Film Cooled Turbine Blade Leading Edge Including Thermal Barrier Coating Effects
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Topics: Coolants , Cooling , Engines , Film cooling , Flow (Dynamics) , Metals , Simulation , Temperature , Thermal barrier coatings , Thermal conductivity
Effect of Wake-Disturbed Flow on Heat (Mass) Transfer to a Turbine Blade
S. Olson, S. Sanitjai, K. Ghosh, R. J. Goldstein
J. Turbomach. January 2011, 133(1): 011015. doi: https://doi.org/10.1115/1.4000538
View articletitled, Effect of Wake-Disturbed Flow on Heat (Mass) Transfer to a Turbine Blade
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Topics: Blades , Flow (Dynamics) , Wakes , Turbulence , Turbine blades , Mass transfer
Casing Treatment and Blade-Tip Configuration Effects on Controlled Gas Turbine Blade Tip/Shroud Rubs at Engine Conditions
Corso Padova, Michael G. Dunn, Jeffery Barton, Kevin Turner, Alan Turner, Darin DiTommaso
J. Turbomach. January 2011, 133(1): 011016. doi: https://doi.org/10.1115/1.4000539
View articletitled, Casing Treatment and Blade-Tip Configuration Effects on Controlled Gas Turbine Blade Tip/Shroud Rubs at Engine Conditions
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Topics: Airfoils , Blades , Stress , Engines , Databases , Gas turbines , Rotors
Reduction of Fan and Compressor Wake Defect Using Plasma Actuation for Tonal Noise Reduction
Sébastien Lemire, Huu Duc Vo
J. Turbomach. January 2011, 133(1): 011017. doi: https://doi.org/10.1115/1.4000540
View articletitled, Reduction of Fan and Compressor Wake Defect Using Plasma Actuation for Tonal Noise Reduction
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Topics: Actuators , Blades , Compressors , Plasmas (Ionized gases) , Wakes , Computational fluid dynamics , Flow (Dynamics) , Rotors , Electrodes , Momentum
Experimental and Numerical Analysis of Gas Turbine Blades With Different Internal Cooling Geometries
M. Eifel, V. Caspary, H. Hönen, P. Jeschke
J. Turbomach. January 2011, 133(1): 011018. doi: https://doi.org/10.1115/1.4000541
View articletitled, Experimental and Numerical Analysis of Gas Turbine Blades With Different Internal Cooling Geometries
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Topics: Blades , Cooling , Flow (Dynamics) , Gas turbines , Heat transfer , Pressure , Water , Vortices , Numerical analysis
Heat Transfer for a Turbine Blade With Nonaxisymmetric Endwall Contouring
Stephen P. Lynch, Narayan Sundaram, Karen A. Thole, Atul Kohli, Christopher Lehane
J. Turbomach. January 2011, 133(1): 011019. doi: https://doi.org/10.1115/1.4000542
View articletitled, Heat Transfer for a Turbine Blade With Nonaxisymmetric Endwall Contouring
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Topics: Blades , Cascades (Fluid dynamics) , Flow (Dynamics) , Heat transfer , Pressure , Vortices , Flow visualization , Reynolds number , Turbine blades
Film Cooling Performance of Converging-Slot Holes With Different Exit-Entry Area Ratios
Cun-liang Liu, Hui-ren Zhu, Jiang-tao Bai, Du-chun Xu
J. Turbomach. January 2011, 133(1): 011020. doi: https://doi.org/10.1115/1.4000543
View articletitled, Film Cooling Performance of Converging-Slot Holes With Different Exit-Entry Area Ratios
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Topics: Film cooling , Discharge coefficient , Heat transfer coefficients , Momentum , Cooling , Liquid crystals , Transients (Dynamics) , Flow (Dynamics) , Heat flux , Turbulence
Concurrent Blade Aerodynamic-Aero-elastic Design Optimization Using Adjoint Method
L. He, D. X. Wang
J. Turbomach. January 2011, 133(1): 011021. doi: https://doi.org/10.1115/1.4000544
View articletitled, Concurrent Blade Aerodynamic-Aero-elastic Design Optimization Using Adjoint Method
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Topics: Blades , Design , Flow (Dynamics) , Optimization , Unsteady flow , Pressure , Flutter (Aerodynamics)
A Study of Mesh-Fed Slot Film Cooling
R. S. Bunker
J. Turbomach. January 2011, 133(1): 011022. doi: https://doi.org/10.1115/1.4000548
View articletitled, A Study of Mesh-Fed Slot Film Cooling
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Topics: Coolants , Cooling , Film cooling , Flow (Dynamics) , Geometry , Airfoils , Wind tunnels
Influence of Stator-Rotor Interaction on the Aerothermal Performance of Recess Blade Tips
Bob Mischo, André Burdet, Reza S. Abhari
J. Turbomach. January 2011, 133(1): 011023. doi: https://doi.org/10.1115/1.4001134
View articletitled, Influence of Stator-Rotor Interaction on the Aerothermal Performance of Recess Blade Tips
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Topics: Blades , Cavities , Flow (Dynamics) , Heat , Rotors , Stators , Stress , Leakage , Heat transfer , Turbines
Computational Study of a Midpassage Gap and Upstream Slot on Vane Endwall Film-Cooling
Satoshi Hada, Karen A. Thole
J. Turbomach. January 2011, 133(1): 011024. doi: https://doi.org/10.1115/1.4001135
View articletitled, Computational Study of a Midpassage Gap and Upstream Slot on Vane Endwall Film-Cooling
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Topics: Combustion chambers , Coolants , Cooling , Film cooling , Flow (Dynamics) , Leakage , Pressure , Suction , Turbines , Design
Assessment of Turbulence Model Predictions for an Aero-Engine Centrifugal Compressor
Jason A. Bourgeois, Robert J. Martinuzzi, Eric Savory, Chao Zhang, Douglas A. Roberts
J. Turbomach. January 2011, 133(1): 011025. doi: https://doi.org/10.1115/1.4001136
View articletitled, Assessment of Turbulence Model Predictions for an Aero-Engine Centrifugal Compressor
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Topics: Compressors , Diffusers , Flow (Dynamics) , Impellers , Pressure , Turbulence , Modeling , Viscosity , Eddies (Fluid dynamics)
Three-Dimensional Aerodynamic Design Optimization of a Turbine Blade by Using an Adjoint Method
Jiaqi Luo, Juntao Xiong, Feng Liu, Ivan McBean
J. Turbomach. January 2011, 133(1): 011026. doi: https://doi.org/10.1115/1.4001166
View articletitled, Three-Dimensional Aerodynamic Design Optimization of a Turbine Blade by Using an Adjoint Method
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Topics: Blades , Boundary-value problems , Design , Flow (Dynamics) , Optimization , Pressure
Analysis of Rotor-Stator-Interaction and Blade-to-Blade Measurements in a Two Stage Axial Flow Compressor
Marco Ernst, Armin Michel, Peter Jeschke
J. Turbomach. January 2011, 133(1): 011027. doi: https://doi.org/10.1115/1.4001168
View articletitled, Analysis of Rotor-Stator-Interaction and Blade-to-Blade Measurements in a Two Stage Axial Flow Compressor
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Topics: Blades , Flow (Dynamics) , Indexing (Machining) , Pressure , Rotors , Stators , Wakes , Vortices , Clearances (Engineering) , Compressors
Experimental and Numerical Investigation of Convective Heat Transfer in a Gas Turbine Can Combustor
Sunil Patil, Santosh Abraham, Danesh Tafti, Srinath Ekkad, Yong Kim, Partha Dutta, Hee-Koo Moon, Ram Srinivasan
J. Turbomach. January 2011, 133(1): 011028. doi: https://doi.org/10.1115/1.4001173
View articletitled, Experimental and Numerical Investigation of Convective Heat Transfer in a Gas Turbine Can Combustor
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Topics: Combustion chambers , Convection , Flow (Dynamics) , Heat transfer , Reynolds number , Turbulence , Gas turbines , Swirling flow , Heat transfer coefficients
A New Alternative for Reduction in Secondary Flows in Low Pressure Turbines
Diego Torre, Raúl Vázquez, Elena de la Rosa Blanco, Howard P. Hodson
J. Turbomach. January 2011, 133(1): 011029. doi: https://doi.org/10.1115/1.4001365
View articletitled, A New Alternative for Reduction in Secondary Flows in Low Pressure Turbines
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Topics: Blades , Computational fluid dynamics , Flow (Dynamics) , Pressure , Turbines , Vortices , Suction , Cascades (Fluid dynamics) , Boundary layers
The Effects of Freestream Turbulence, Turbulence Length Scale, and Exit Reynolds Number on Turbine Blade Heat Transfer in a Transonic Cascade
J. S. Carullo, S. Nasir, R. D. Cress, W. F. Ng, K. A. Thole, L. J. Zhang, H. K. Moon
J. Turbomach. January 2011, 133(1): 011030. doi: https://doi.org/10.1115/1.4001366
View articletitled, The Effects of Freestream Turbulence, Turbulence Length Scale, and Exit Reynolds Number on Turbine Blade Heat Transfer in a Transonic Cascade
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Topics: Blades , Heat transfer , Pressure , Turbulence , Reynolds number , Flow (Dynamics) , Mach number , Cascades (Fluid dynamics)
Thermomechanical Transient Analysis and Conceptual Optimization of a First Stage Bucket
Alfonso Campos-Amezcua, Zdzislaw Mazur-Czerwiec, Armando Gallegos-Muñoz
J. Turbomach. January 2011, 133(1): 011031. doi: https://doi.org/10.1115/1.4001367
View articletitled, Thermomechanical Transient Analysis and Conceptual Optimization of a First Stage Bucket
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Topics: Blades , Heat transfer , Optimization , Stress , Temperature , Thermomechanics , Transient analysis , Turbines , Computational fluid dynamics , Finite element analysis
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Unsteady Flow Structure of Rotating Instability in a 1.5-Stage Axial Compressor
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Performance of Rough-Ribbed Low-Pressure Turbine Blades Under Varying Loading and Operating Conditions
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CONTROL OF SHROUD LEAKAGE LOSS AND WINDAGE TORQUE IN A LOW-PRESSURE TURBINE STAGE
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Numerical implementation of electrostatic solver within OpenFOAM for GT intake filtration
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  • Print ISSN 0889-504X

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