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Proceedings Papers

Proceedings Volume Cover
ASME Turbo Expo 2013: Turbine Technical Conference and Exposition
June 3–7, 2013
San Antonio, Texas, USA
Conference Sponsors:
  • International Gas Turbine Institute
ISBN:
978-0-7918-5516-4
Volume 3C: Heat Transfer

General Interest

Comparison of Temperature Profile and Heat Transfer Predictions With Statistically-Modeled Data From a Cooled 1-1/2 Stage High-Pressure Transonic Turbine
Harika S. Kahveci, Kevin R. Kirtley
GT 2013; V03CT14A001https://doi.org/10.1115/GT2013-94242
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Topics: Heat transfer , High pressure (Physics) , Temperature profiles , Turbines , Uncertainty , Blades , Computational fluid dynamics , Cooling , Gages , Surface roughness
Gas Turbine Cooling: Moving From Macro to Micro Cooling
Ronald S. Bunker
GT 2013; V03CT14A002https://doi.org/10.1115/GT2013-94277
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Topics: Cooling , Gas turbines , Turbines , Airfoils , Flow (Dynamics) , Durability , Dust , Film cooling , Fluids , High pressure (Physics)
Wall Temperature Effects on Heat Transfer Coefficient
Roberto Maffulli, Li He
GT 2013; V03CT14A003https://doi.org/10.1115/GT2013-94291
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Topics: Heat transfer coefficients , Wall temperature , Blades , Heat transfer , Nozzle guide vanes , Aerodynamics , Boundary layers , Computation , Computational fluid dynamics , Fluids
The Effect of Axisymmetric Profile on Turbine Blade Platform Heat Transfer Distribution
Luzeng Zhang, Dong H. Lee, Juan Yin, Hee Koo Moon
GT 2013; V03CT14A004https://doi.org/10.1115/GT2013-94335
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Topics: Heat transfer , Turbine blades , Flow (Dynamics) , Blades , Cascades (Fluid dynamics) , Engines , Heat , Reynolds number , Shapes , Stress
Effects of Tip Clearance Gap and Exit Mach Number on Turbine Blade Tip and Near-Tip Heat Transfer
K. Anto, S. Xue, W. F. Ng, L. J. Zhang, H. K. Moon
GT 2013; V03CT14A005https://doi.org/10.1115/GT2013-94345
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Topics: Clearances (Engineering) , Heat transfer , Mach number , Turbine blades , Blades , Suction , Pressure , Cascades (Fluid dynamics) , Engines , Leakage
Experimental Investigation Into Thermal Behavior of Steam Turbine Components: Part 3 — Startup and the Impact on LCF Life
Gabriel Marinescu, Michael Sell, Andreas Ehrsam, Philipp B. Brunner
GT 2013; V03CT14A006https://doi.org/10.1115/GT2013-94356
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Topics: Steam turbines , Steam , Electrical conductivity , Flow (Dynamics) , Fluids , High temperature , Rotors , Thermal conductivity , Turbines , Cavities
An Inverse Heat Transfer Approach to Mitigating Sources of Experimental Error in Transient Heat Transfer Experiments
James L. Rutledge, Jonathan F. McCall
GT 2013; V03CT14A007https://doi.org/10.1115/GT2013-94583
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Topics: Errors , Heat transfer , Heat transfer coefficients , Transient heat transfer , Transients (Dynamics)
Direct Measurements of Overall Effectiveness and Heat Flux on a Film Cooled Test Article at High Temperatures and Pressures
S. A. Lawson, D. L. Straub, S. Beer, K. H. Casleton, T. Sidwell
GT 2013; V03CT14A008https://doi.org/10.1115/GT2013-94685
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Topics: Heat flux , High temperature , Gas turbines , Gases , Integrated gasification combined cycle power stations , Pressure , Thermography , Wall temperature , Combined cycles , Cooling
The Concept of Adiabatic Heat Transfer Coefficient and its Application to Turbomachinery
Reinaldo A. Gomes, Reinhard Niehuis
GT 2013; V03CT14A009https://doi.org/10.1115/GT2013-94715
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Topics: Heat transfer coefficients , Turbomachinery , Boundary-value problems , Flow (Dynamics) , Temperature , Aerodynamics , Design , Heat flux , Thermal boundary layers , Turbine blades
A Review of the AFRL Turbine Research Facility
Richard J. Anthony, John P. Clark
GT 2013; V03CT14A010https://doi.org/10.1115/GT2013-94741
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Topics: Turbines , Testing , Engines , Heat transfer , Aerodynamics , Air Force , Airfoils , Computational fluid dynamics , Construction , Design
Blade Tip Shape Optimization for Enhanced Turbine Aerothermal Performance
C. De Maesschalck, S. Lavagnoli, G. Paniagua
GT 2013; V03CT14A011https://doi.org/10.1115/GT2013-94754
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Topics: Blades , Shape optimization , Turbines , Flow (Dynamics) , Leakage flows , Optimization , Shapes , Stress , Rotors , Aerodynamics
Validation of Surface Pressure Predictions for Nozzle Airfoil and Endwall Film Cooling Design Using Transonic Cascade Measurements
Jason E. Dees, James A. Tallman, Michael A. Heminger, Daniel Wilde
GT 2013; V03CT14A012https://doi.org/10.1115/GT2013-94921
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Topics: Airfoils , Cascades (Fluid dynamics) , Design , Film cooling , Nozzles , Pressure , Computational fluid dynamics , Pressure measurement , Engines , Flow (Dynamics)
History of Short-Duration Measurement Programs Related to Gas Turbine Heat Transfer, Aerodynamics, and Aeroperformance at Calspan and OSU
Michael Dunn, Randall Mathison
GT 2013; V03CT14A013https://doi.org/10.1115/GT2013-94926
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Topics: Aerodynamics , Gas turbines , Heat transfer , Turbines , Flow (Dynamics) , Blades , Cooling , Aviation , Heat flux , Pressure
A CFD Evaluation of Multiple RANS Turbulence Models for Prediction of Boundary Layer Flows on a Turbine Vane
Thomas E. Dyson, David G. Bogard, Sean D. Bradshaw
GT 2013; V03CT14A014https://doi.org/10.1115/GT2013-94927
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Topics: Boundary layers , Computational fluid dynamics , Flow (Dynamics) , Reynolds-averaged Navier–Stokes equations , Turbines , Turbulence , Thermal boundary layers , Prandtl number , Cooling , Engineering simulation
Endwall Heat Transfer for a Turbine Blade With an Upstream Cavity and Rim Seal Leakage
Stephen P. Lynch, Karen A. Thole, Atul Kohli, Christopher Lehane, Tom Praisner
GT 2013; V03CT14A015https://doi.org/10.1115/GT2013-94942
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Topics: Cavities , Heat transfer , Leakage , Turbine blades , Flow (Dynamics) , Blades , Leakage flows , Vortex flow , Airfoils , Clearances (Engineering)
Characterization of Flow Through Porous Metals
Michael J. Hargather, Karen A. Thole
GT 2013; V03CT14A016https://doi.org/10.1115/GT2013-94945
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Topics: Flow (Dynamics) , Metals , Pressure drop , Compressible flow , Density , Flow measurement , Internal flow , Nozzles , Porosity , Porous materials
Endwall Heat Transfer Measurements of an Outlet Guide Vane at On and Off Design Conditions
Lei Wang, Bengt Sundén, Valery Chernoray, Hans Abrahamsson
GT 2013; V03CT14A017https://doi.org/10.1115/GT2013-95008
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Topics: Design , Guide vanes , Heat transfer , Flow separation , Cascades (Fluid dynamics) , Computational fluid dynamics , Flow (Dynamics) , Heat transfer coefficients , Liquid crystals , Reynolds number
A Simplified Model to Assess the Influence of Load Ramps on the Durability of Hot Gas Path Components in Heavy-Duty Gas Turbines
Alessandro D. Ramaglia, Luca Bozzi
GT 2013; V03CT14A018https://doi.org/10.1115/GT2013-95009
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Topics: Durability , Gas turbines , Stress , Blades , Cooling , Temperature gradient , Cycles , Design , Engines , Materials testing
The Development of a Closed Loop High Speed Cascade Wind Tunnel for Aerodynamic and Heat Transfer Testing at Moderate to Low Reynolds Numbers
M. P. Mihelish, F. E. Ames
GT 2013; V03CT14A019https://doi.org/10.1115/GT2013-95048
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Topics: Cascades (Fluid dynamics) , Heat transfer , Reynolds number , Testing , Wind tunnels , Engines , Flow (Dynamics) , Chords (Trusses) , Mach number , Turbines
The Response of High Intensity Turbulence in the Presence of Large Stagnation Regions
N. Chowdhury, F. E. Ames
GT 2013; V03CT14A020https://doi.org/10.1115/GT2013-95055
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Topics: Turbulence , Flow (Dynamics) , Spectra (Spectroscopy) , Eddies (Fluid dynamics) , Energy dissipation , Convection , Cylinders , Elongation , Gas turbines , Heat
Cooling of a Honeycomb Shroud Seal in Order to Reduce Oxidation
A. W. Davis, A. Dawson, L. Bunn, A. Bonaldo, M. Hill, C. F. Favaretto, R. Backhouse
GT 2013; V03CT14A021https://doi.org/10.1115/GT2013-95061
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Topics: Cooling , Honeycomb structures , Oxidation , Engines , Computational fluid dynamics , Blades , Cavities , Flow (Dynamics) , Temperature , Gas turbines
Deposition With Hot Streaks in an Uncooled Turbine Vane Passage
B. Casaday, R. Prenter, C. Bonilla, M. Lawrence, C. Clum, A. Ameri, J. P. Bons
GT 2013; V03CT14A022https://doi.org/10.1115/GT2013-95108
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Topics: Turbines , Particulate matter , Flow (Dynamics) , Temperature , Cascades (Fluid dynamics) , Engineering simulation , High pressure (Physics) , Jets , Simulation , Trajectories (Physics)
A Study of the Heat Transfer in Winglet and Squealer Rotor Tip Configurations for a Non-Cooled HPT Blade Based on CFD Calculations
Lucilene Moraes da Silva, Jesuino Takachi Tomita
GT 2013; V03CT14A023https://doi.org/10.1115/GT2013-95164
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Topics: Blades , Computational fluid dynamics , Heat transfer , Rotors , Flow (Dynamics) , Design , Leakage , Turbines , Energy conservation , Energy transformation
Manufacturing Influences on Pressure Losses of Channel Fed Holes
Michael Barringer, Karen A. Thole, Vaidyanathan Krishnan, Evan Landrum
GT 2013; V03CT14A024https://doi.org/10.1115/GT2013-95236
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Topics: Manufacturing , Pressure , Flow (Dynamics) , Reynolds number , Channel flow , Cooling , Engines , Film cooling , Friction , Impingement cooling
Advanced Flow Control for Supersonic Blowdown Wind Tunnel Using Extended Kalman Filter
Jiaqi Xi, Qiang Zhang, Mian Li, Zhaoguang Wang
GT 2013; V03CT14A025https://doi.org/10.1115/GT2013-95281
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Topics: Flow control , Kalman filters , Wind tunnels
A Review of the Oxford Turbine Research Facility
Kam Chana, Dave Cardwell, Terry Jones
GT 2013; V03CT14A026https://doi.org/10.1115/GT2013-95687
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Topics: Turbines , Cooling , Gas turbines , Heat transfer , Cascades (Fluid dynamics) , Pistons , Blades , Design , Experimental methods , Flow (Dynamics)
Unsteady, Half-Annulus CFD Calculations of Thermal Migration Through a Cooled, 2.5 Stage High-Pressure Turbine
James A. Tallman
GT 2013; V03CT14A027https://doi.org/10.1115/GT2013-95823
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Topics: Annulus , Computational fluid dynamics , High pressure (Physics) , Turbines , Airfoils , Engines , Flow (Dynamics) , Aviation , Blades , Cavities
Large-Eddy Simulation for Turbine Heat Transfer
Gorazd Medic, Jongwook Joo, Ivana Milanovic, Om Sharma
GT 2013; V03CT14A028https://doi.org/10.1115/GT2013-95841
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Topics: Heat transfer , Large eddy simulation , Turbines , Stators , Turbulence , Flow (Dynamics) , Rotors , Pressure , Blades , Flow separation
Experimental Analysis of Flow Unbalance in Two Parallel Counter-Flow Recuperators
Alessio Martini, Alberto Traverso, David Tucker, John VanOsdol
GT 2013; V03CT14A029https://doi.org/10.1115/GT2013-95886
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Topics: Experimental analysis , Flow (Dynamics) , Valves , Heat exchangers , Stress , Symmetry (Physics) , Air compressors , Exhaust systems , Fuels , Heat
The Challenges of Uniform Crystal Temperature Sensor (UCTS) Application in Turbomachinery
Justin Brown, Jason DeVoe, Lev Ginzbursky
GT 2013; V03CT14A030https://doi.org/10.1115/GT2013-95909
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Topics: Crystals , Temperature sensors , Turbomachinery , Engines , Design , Engineers , Finite element analysis , Instrumentation , Boundary-value problems , Collaboration
Review of the von Karman Institute Compression Tube Facility for Turbine Research
G. Paniagua, C. H. Sieverding, T. Arts
GT 2013; V03CT14A031https://doi.org/10.1115/GT2013-95984
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Topics: Compression , Turbines , Cooling , Flow (Dynamics) , Gas turbines , Heat transfer , Design , Electronics , Engines , Experimental methods

Combustors (With Combustion, Fuels and Emissions)

Experimental Study of the Flow and Pressure Drop Performances in Advanced Combustor Distributor Diffuser
H. X. Liang, J. Q. Suo, M. Li
GT 2013; V03CT17A001https://doi.org/10.1115/GT2013-94209
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Topics: Combustion chambers , Diffusers , Flow (Dynamics) , Gas turbines , Pressure , Pressure drop
Investigation of the Effect of Perforated Sheath on Thermal-Flow Characteristics Over a Gas Turbine Reverse-Flow Combustor: Part 1 — Experiment
Liang Wang, Ting Wang
GT 2013; V03CT17A002https://doi.org/10.1115/GT2013-94474
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Topics: Combustion chambers , Flow (Dynamics) , Gas turbines , Pressure , Temperature , Cooling , Diffusers , Channel flow , Coating processes , Coatings
Investigation of the Effect of Perforated Sheath on Thermal-Flow Characteristics Over a Gas Turbine Reverse-Flow Combustor: Part 2 — Computational Analysis
Liang Wang, Ting Wang
GT 2013; V03CT17A003https://doi.org/10.1115/GT2013-94475
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Topics: Combustion chambers , Flow (Dynamics) , Gas turbines , Pressure , Temperature , Diffusers , Wall temperature , Advanced materials , Cavities , Coatings
Experimental and Theoretical Investigation of Thermal Effectiveness in Multi-Perforated Plates for Combustor Liner Effusion Cooling
Antonio Andreini, Bruno Facchini, Alessio Picchi, Lorenzo Tarchi, Fabio Turrini
GT 2013; V03CT17A004https://doi.org/10.1115/GT2013-94667
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Topics: Combustion chambers , Cooling , Plates (structures) , Coolants , Cooling systems , Engineering simulation , Engines , Film cooling , Fluids , Forced convection
Effect of Variable Properties Within a Boundary Layer With Large Freestream to Wall Temperature Differences
Nathan J. Greiner, Marc D. Polanka, Jacob R. Robertson, James L. Rutledge
GT 2013; V03CT17A005https://doi.org/10.1115/GT2013-94794
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Topics: Boundary layers , Wall temperature , Temperature , Turbines , Blades , Combustion chambers , Flow (Dynamics) , Aviation , Convection , Cooling
Local Source Based CFD Modeling of Effusion Cooling Holes: Validation and Application to an Actual Combustor Test Case
A. Andreini, R. Da Soghe, B. Facchini, L. Mazzei, S. Colantuoni, F. Turrini
GT 2013; V03CT17A006https://doi.org/10.1115/GT2013-94874
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Topics: Combustion chambers , Computational fluid dynamics , Cooling , Modeling , Coolants , Flow (Dynamics) , Heat sinks , Discharge coefficient , Engineering simulation , Film cooling
Numerical Analysis of Effusion Plates for Combustor Liners Cooling With Varying Density Ratio
L. Andrei, A. Andreini, C. Bianchini, B. Facchini, L. Mazzei
GT 2013; V03CT17A007https://doi.org/10.1115/GT2013-95039
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Topics: Combustion chambers , Cooling , Density , Numerical analysis , Plates (structures) , Turbulence , Acoustical properties , Aircraft engines , Algebra , Anisotropy
Numerical Prediction of NOx Emission and Exit Temperature Pattern in a Model Staged Lean Premixed Prevaporized Combustor
Man Zhang, Hao Wu, Hao Wang
GT 2013; V03CT17A008https://doi.org/10.1115/GT2013-95235
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Topics: Combustion chambers , Emissions , Nitrogen oxides , Temperature , Combustion , Flames , Temperature distribution , Turbulence , Air flow , Aircraft engines
Development of an Annular Combustor Chamber
Uwe Ruedel, Bogdan Trbojevic, Urs Benz, Martin Zajadatz, Klaus Doebbeling
GT 2013; V03CT17A009https://doi.org/10.1115/GT2013-95495
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Topics: Combustion chambers , Design , Combustion , Cooling , Engines , Gas turbines , Inspection , Emissions , Energy generation , Fuels
Design of a Non-Reacting Combustor Simulator With Swirl and Temperature Distortion With Experimental Validation
Benjamin F. Hall, Kam S. Chana, Thomas Povey
GT 2013; V03CT17A010https://doi.org/10.1115/GT2013-95499
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Topics: Combustion chambers , Design , Temperature , Flow (Dynamics) , Aerodynamics , Heat , Vortices , Low temperature , Rotors , Stress

Structures (With Structures and Dynamics)

Temperature-Based Optimization of Film Cooling in Gas Turbine Hot Gas Path Components
Felipe A. C. Viana, Jack Madelone, Niranjan Pai, Genghis Khan, Sanghum Baik
GT 2013; V03CT18A001https://doi.org/10.1115/GT2013-94293
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Topics: Film cooling , Gas turbines , Optimization , Temperature , Cooling , Flow (Dynamics) , Design , Metals , Alloys , Approximation
Gas Turbines and Uncertainty Quantification: Impact of PDF Tails on UQ Predictions, the Black Swan
Francesco Montomoli, Michela Massini
GT 2013; V03CT18A002https://doi.org/10.1115/GT2013-94306
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Topics: Gas turbines , Uncertainty quantification , Probability , Computational fluid dynamics , Design , Uncertainty , Failure , Gaussian distribution , Geometry , Simulation
Adaptive Flow Field Thermal Modeling Techniques for Turbine Rotor-Stator Cavities
Jose Maria Rey Villazón, Martin Berthold, Arnold Kühhorn
GT 2013; V03CT18A003https://doi.org/10.1115/GT2013-94845
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Topics: Cavities , Flow (Dynamics) , Modeling , Rotors , Stators , Turbines , Computational fluid dynamics , Design , Disks , Boundary-value problems
The Use of Probabilistic Methods in Determining Turbine Disc Cyclic Life Uncertainty
David T. Williams, Peter Smout, Matteo Bianchi, Martin B. Joinson
GT 2013; V03CT18A004https://doi.org/10.1115/GT2013-94972
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Topics: Disks , Turbines , Uncertainty , Gas turbines , Engines , Modeling , Aircraft , Temperature , Cycles , Engine design
Performance Analysis of a Rotating Labyrinth Seal With Radial Growth
Sivakumar Subramanian, A. S. Sekhar, B. V. S. S. S. Prasad
GT 2013; V03CT18A005https://doi.org/10.1115/GT2013-95708
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Topics: Clearances (Engineering) , Deformation , Leakage flows , Pressure , Rotation
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