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Proceedings Papers

Proceedings Volume Cover
ASME Turbo Expo 2000: Power for Land, Sea, and Air
May 8–11, 2000
Munich, Germany
Conference Sponsors:
  • International Gas Turbine Institute
ISBN:
978-0-7918-7856-9
In This Volume
Volume 3: Heat Transfer; Electric Power; Industrial and Cogeneration

Heat Transfer

Leakage Flow Over Shrouded Turbine Blades
Yumin Xiao, R. S. Amano
GT 2000; V003T01A001https://doi.org/10.1115/2000-GT-0193
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Topics: Leakage flows , Turbine blades , Flow (Dynamics) , Pressure , Navier-Stokes equations , Turbulence
Heat Transfer and Pressure Distributions on a Gas Turbine Blade Tip
Gm S. Azad, Je-Chin Han, Shuye Teng, Robert J. Boyle
GT 2000; V003T01A002https://doi.org/10.1115/2000-GT-0194
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Topics: Blades , Gas turbines , Heat transfer , Pressure , Heat transfer coefficients , Cascades (Fluid dynamics) , Clearances (Engineering) , Rotors , Turbulence , Aircraft
Heat Transfer and Flow on the Squealer Tip of a Gas Turbine Blade
Gm S. Azad, Je-Chin Han, Robert J. Boyle
GT 2000; V003T01A003https://doi.org/10.1115/2000-GT-0195
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Topics: Blades , Flow (Dynamics) , Gas turbines , Heat transfer , Heat transfer coefficients , Cavities , Cascades (Fluid dynamics) , Pressure , Turbulence , Rotors
Experimental Investigations on the Thermal Load and Leakage Flow of a Turbine Blade Tip Section With Different Tip Section Geometries
Martin F. Urban, Nicolas Vortmeyer
GT 2000; V003T01A004https://doi.org/10.1115/2000-GT-0196
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Topics: Leakage flows , Stress , Turbine blades , Blades , Flow (Dynamics) , Steam , Cascades (Fluid dynamics) , Chords (Trusses) , Combustion , Coolants
Time-Averaged Heat Flux for a Recessed Tip, Lip, and Platform of a Transonic Turbine Blade
M. G. Dunn, C. W. Haldeman
GT 2000; V003T01A005https://doi.org/10.1115/2000-GT-0197
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Topics: Heat flux , Turbine blades , Blades , Pressure , Suction , Turbines , Chords (Trusses) , Design , Flow (Dynamics) , Heat transfer
Flow and Heat Transfer at the Hub Endwall of Inlet Vane Passages — Experiments and Simulations
R. P. Roy, K. D. Squires, M. Gerendas, S. Song, W. J. Howe, A. Ansari
GT 2000; V003T01A006https://doi.org/10.1115/2000-GT-0198
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Topics: Engineering simulation , Flow (Dynamics) , Heat transfer , Simulation , Turbulence , Cascades (Fluid dynamics) , Computer simulation , Heat flux , Liquid crystals , Momentum
Effects of Slot Bleed Injection Over a Contoured Endwall on Nozzle Guide Vane Cooling Performance: Part I — Flow Field Measurements
Steven W. Burd, Terrence W. Simon
GT 2000; V003T01A007https://doi.org/10.1115/2000-GT-0199
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Topics: Cooling , Flow (Dynamics) , Nozzle guide vanes , Cascades (Fluid dynamics) , Combustion chambers , Airfoils , Nozzles , Turbines , Turbulence , Chords (Trusses)
Effects of Slot Bleed Injection Over a Contoured End Wall on Nozzle Guide Vane Cooling Performance: Part II — Thermal Measurements
Steven W. Burd, Cynthia J. Satterness, Terrence W. Simon
GT 2000; V003T01A008https://doi.org/10.1115/2000-GT-0200
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Topics: Cooling , Nozzle guide vanes , Flow (Dynamics) , Airfoils , Combustion chambers , Coolants , Cascades (Fluid dynamics) , Chords (Trusses) , Convection , Design
High Freestream Turbulence Effects on Endwall Heat Transfer for a Gas Turbine Stator Vane
R. W. Radomsky, K. A. Thole
GT 2000; V003T01A009https://doi.org/10.1115/2000-GT-0201
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Topics: Gas turbines , Heat transfer , Stators , Turbulence , Vortices , Convection , Flow (Dynamics) , Airfoils , Combustion chambers , Geometry
An Investigation of Heat Transfer in a Film Cooled Transonic Turbine Cascade: Part I — Steady Heat Transfer
D. E. Smith, J. V. Bubb, O. Popp, H. Grabowski, III, T. E. Diller, J. A. Schetz, W. F. Ng
GT 2000; V003T01A010https://doi.org/10.1115/2000-GT-0202
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Topics: Cascades (Fluid dynamics) , Heat transfer , Turbines , Gages , Blades , Coolants , Film cooling , Heat transfer coefficients , Cooling , Pressure
Investigation of Heat Transfer in a Film Cooled Transonic Turbine Cascade: Part II — Unsteady Heat Transfer
O. Popp, D. E. Smith, J. V. Bubb, H. C. Grabowski, III, T. E. Diller, J. A. Schetz, W. F. Ng
GT 2000; V003T01A011https://doi.org/10.1115/2000-GT-0203
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Topics: Cascades (Fluid dynamics) , Heat transfer , Turbines , Blades , Shock waves , Rotors , Shock (Mechanics) , Suction , Film cooling , Heat flux
Influence of Surface Roughness on Heat Transfer and Effectiveness for a Fully Film Cooled Nozzle Guide Vane Measured by Wide Band Liquid Crystals and Direct Heat Flux Gauges
S. M. Guo, C. C. Lai, T. V. Jones, M. L. G. Oldfield, G. D. Lock, A. J. Rawlinson
GT 2000; V003T01A012https://doi.org/10.1115/2000-GT-0204
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Topics: Gages , Heat flux , Heat transfer , Liquid crystals , Nozzle guide vanes , Surface roughness , Heat transfer coefficients , Cooling , Engines , Film cooling
The Influence of the Boundary Layer State and Reynolds Number on Film Cooling and Heat Transfer on a Cooled Nozzle Guide Vane
Hans Reiss, Albin Bölcs
GT 2000; V003T01A013https://doi.org/10.1115/2000-GT-0205
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Topics: Boundary layers , Film cooling , Heat transfer , Nozzle guide vanes , Reynolds number , Flow (Dynamics) , Suction , Heat transfer coefficients , Aerodynamic flow , Airfoils
Influence of Vane/Blade Spacing on the Heat Flux for a Transonic Turbine
M. G. Dunn, C. W. Haldeman, R. S. Abhari, M. L. McMillan
GT 2000; V003T01A014https://doi.org/10.1115/2000-GT-0206
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Topics: Blades , Heat flux , Turbines , Pressure , Chords (Trusses) , Heat , Reynolds number , Stress
Cooling Effectiveness Measurements With Thermal Radiometry in a Turbine Cascade
H. K. Moon, R. Jaiswal
GT 2000; V003T01A015https://doi.org/10.1115/2000-GT-0207
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Topics: Cascades (Fluid dynamics) , Cooling , Radiation measurement , Turbines , Airfoils , Temperature , Coolants , Engines , Thermocouples , Background radiation
Rotor / Stator Heat Transfer Measurements and CFD Predictions for Short-Duration Turbine Rig Tests
Robert F. Bergholz, Michael G. Dunn, Gary D. Steuber
GT 2000; V003T01A016https://doi.org/10.1115/2000-GT-0208
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Topics: Computational fluid dynamics , Heat transfer , Rotors , Stators , Turbines , Blades , Airfoils , Heat flux , Uncertainty , Gages
Heat Transfer Measurements and Predictions on a Power Generation Gas Turbine Blade
Paul W. Giel, Ronald S. Bunker, G. James Van Fossen, Robert J. Boyle
GT 2000; V003T01A017https://doi.org/10.1115/2000-GT-0209
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Topics: Blades , Energy generation , Gas turbines , Heat transfer , Design , Reynolds number , Turbulence , Airfoils , Boundary layers , Cascades (Fluid dynamics)
Aerodynamics and Heat Transfer in a Turbine Blade at Design and Off-Design Angles of Incidence
C. Xu, R. S. Amano
GT 2000; V003T01A018https://doi.org/10.1115/2000-GT-0210
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Topics: Aerodynamics , Design , Heat transfer , Turbine blades , Flow (Dynamics) , Navier-Stokes equations , Numerical analysis , Algorithms , Blades , Momentum
Analysis of Flow and Heat Transfer in the End-Wall Region of a Turbine Blade Passage
Yumin Xiao, R. S. Amano
GT 2000; V003T01A019https://doi.org/10.1115/2000-GT-0211
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Topics: Flow (Dynamics) , Heat transfer , Turbine blades , Vortices , Corners (Structural elements) , Blades , Turbulence , Wakes , Algebra
Secondary Flow Measurements in a Turbine Passage With Endwall Flow Modification
Nicole V. Aunapu, Ralph J. Volino, Karen A. Flack, Ryan M. Stoddard
GT 2000; V003T01A020https://doi.org/10.1115/2000-GT-0212
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Topics: Flow (Dynamics) , Flow measurement , Turbines , Jets , Blades , Vortices , Boundary layers , Cascades (Fluid dynamics) , Film cooling , Flow visualization
Flow Measurements in a Nozzle Guide Vane Passage With a Low Aspect Ratio and Endwall Contouring
Steven W. Burd, Terrence W. Simon
GT 2000; V003T01A021https://doi.org/10.1115/2000-GT-0213
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Topics: Flow measurement , Nozzle guide vanes , Cascades (Fluid dynamics) , Flow (Dynamics) , Airfoils , Arches , Heat transfer , Hydrodynamics , Pressure gradient , Pressure measurement
Measurements in a Turbine Cascade Over a Contoured Endwall: Discrete Hole Injection of Bleed Flow
Rohit A. Oke, Terrence W. Simon, Steven W. Burd, Rickard Vahlberg
GT 2000; V003T01A022https://doi.org/10.1115/2000-GT-0214
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Topics: Cascades (Fluid dynamics) , Flow (Dynamics) , Turbines , Coolants , Airfoils , Suction , Cooling , Cross-flow , Engines , Momentum
Augmentation of Stagnation Region Heat Transfer due to Turbulence From a DLN Can Combustor
G. James Van Fossen, Ronald S. Bunker
GT 2000; V003T01A023https://doi.org/10.1115/2000-GT-0215
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Topics: Combustion chambers , Heat transfer , Turbulence , Flow (Dynamics) , Fuels , Wire , Air flow , Aluminum , Flat plates , Heat transfer coefficients
Infrared Low Temperature Turbine Vane Rough Surface Heat Transfer Measurements
R. J. Boyle, C. M. Spuckler, B. L. Lucci, W. P. Camperchioli
GT 2000; V003T01A024https://doi.org/10.1115/2000-GT-0216
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Topics: Heat transfer , Low temperature , Surface roughness , Turbines , Cascades (Fluid dynamics) , Heat conduction , Mach number , Pressure , Suction , Temperature
Comparison of Predicted and Measured Turbine Vane Rough Surface Heat Transfer
R. J. Boyle, C. M. Spuckler, B. L. Lucci
GT 2000; V003T01A025https://doi.org/10.1115/2000-GT-0217
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Topics: Heat transfer , Surface roughness , Turbines , Turbulence , Algebra , Reynolds number , Accounting , Boundary-value problems , Mach number
The Two-Flux Model Applied to Radiative Transfer and Forced Convection in the Laminar Boundary Layer on a Flat Plate
Freddy Malpica, Nathaly Moreno, Andrés Tremante
GT 2000; V003T01A026https://doi.org/10.1115/2000-GT-0218
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Topics: Boundary layers , Flat plates , Forced convection , Radiative heat transfer , Radiation (Physics) , Convection , Heat transfer , Thermal boundary layers , Blades , Compressors
Heat Transfer and Flow Characteristics of an Engine Representative Impingement Cooling System
Changmin Son, David Gillespie, Peter Ireland, Geoffrey M. Dailey
GT 2000; V003T01A027https://doi.org/10.1115/2000-GT-0219
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Topics: Engines , Flow (Dynamics) , Heat transfer , Impingement cooling , Liquid crystals , Pressure , Coatings , Energy budget (Physics) , Engineering standards , Flow visualization
Experimental Investigation on Impingement Heat Transfer From Rib Roughened Surface Within Arrays of Circular Jets: Correlation
Haiping Chang, Jingyu Zhang, Taiping Huang
GT 2000; V003T01A028https://doi.org/10.1115/2000-GT-0220
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Topics: Heat transfer , Jets , Cooling , Guide vanes , Blades , Flow (Dynamics) , Gas turbines , High temperature , Polynomials , Turbine blades
Mist/Steam Heat Transfer in Confined Slot Jet Impingement
X. Li, J. L. Gaddis, T. Wang
GT 2000; V003T01A029https://doi.org/10.1115/2000-GT-0221
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Topics: Heat transfer , Steam , Cooling , Reynolds number , Blades , Drops , Flux (Metallurgy) , Heat , Turbines , Wall temperature
An Experimental Evaluation of Advanced Leading Edge Impingement Cooling Concepts
M. E. Taslim, L. Setayeshgar, S. D. Spring
GT 2000; V003T01A030https://doi.org/10.1115/2000-GT-0222
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Topics: Airfoils , Blades , Cavities , Convection , Cooling , Flow (Dynamics) , Heat transfer , Heat transfer coefficients , Impingement cooling , Jets
Flow and Heat Transfer of Confined Impingement Jets Cooling
Ting Wang, Mingjie Lin, Ronald S. Bunker
GT 2000; V003T01A031https://doi.org/10.1115/2000-GT-0223
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Topics: Cooling , Flow (Dynamics) , Heat transfer , Jets , Heat transfer coefficients , Reynolds number , Cavities , Convection , Cross-flow , Liquid crystals
Heat Transfer in Rotating Narrow Rectangular Ducts With Heated Sides Oriented at 60° to the r-z Plane
Fred T. Willett, Arthur E. Bergles
GT 2000; V003T01A032https://doi.org/10.1115/2000-GT-0224
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Topics: Ducts , Heat transfer , Rotation , Cavities , Blades , Cooling , Engines , Gas turbines , Heat flux , Heat transfer coefficients
Application of Non-Linear k–ω Model to the Turbulent Flow Inside a Sharp U-Bend
B. Song, R. S. Amano
GT 2000; V003T01A033https://doi.org/10.1115/2000-GT-0225
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Topics: Turbulence , Flow (Dynamics) , Anisotropy , Ducts , Interpolation , Shear stress , Simulation
Heat Transfer Enhancements in Rotating Two-Pass Coolant Channels With Profiled Ribs: Part 2 — Detailed Measurements
D. E. Nikitopoulos, V. Eliades, S. Acharya
GT 2000; V003T01A034https://doi.org/10.1115/2000-GT-0226
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Topics: Coolants , Heat transfer , Mass transfer , Heat , Reynolds number , Rotation
Heat Transfer Enhancements in Rotating Two-Pass Coolant Channels With Profiled Ribs: Part 1 — Average Results
S. Acharya, V. Eliades, D. E. Nikitopoulos
GT 2000; V003T01A035https://doi.org/10.1115/2000-GT-0227
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Topics: Coolants , Heat transfer , Ducts , Heat , Flow (Dynamics) , Gas turbines , Reynolds number , Rotation , Vorticity
Rotating Effect on Fluid Flow in a Smooth Duct With a 180-Deg Sharp Turn
Chung-Chu Chen, Tong-Miin Liou
GT 2000; V003T01A036https://doi.org/10.1115/2000-GT-0228
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Topics: Ducts , Fluid dynamics , Heat transfer , Turbulence , Flow (Dynamics) , Vortices , Kinetic energy , Blades , Coolants , Fluids
Flow and Heat Transfer in a Rotating Square Channel With 45° Angled Ribs by Reynolds Stress Turbulence Model
Yong-Jun Jang, Hamn -Ching Chen, Je-Chin Han
GT 2000; V003T01A037https://doi.org/10.1115/2000-GT-0229
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Topics: Flow (Dynamics) , Heat transfer , Stress , Turbulence , Buoyancy , Computation , Coolants , Coriolis force , Corners (Structural elements) , Density
Local Heat Transfer and Flow Structure on and Above a Dimpled Surface in a Channel
G. I. Mahmood, M. L. Hill, D. L. Nelson, P. M. Ligrani, H.-K. Moon, B. Glezer
GT 2000; V003T01A038https://doi.org/10.1115/2000-GT-0230
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Topics: Flow (Dynamics) , Heat transfer , Fluids , Temperature , Vortices , Flow visualization , Calibration , Pressure , Reynolds number , Thermocouples
A Transient Liquid Crystal Method Using Hue Angle and a 3-D Inverse Transient Conduction Scheme
Mingjie Lin, Ting Wang
GT 2000; V003T01A039https://doi.org/10.1115/2000-GT-0231
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Topics: Liquid crystals , Transient heat transfer , Transients (Dynamics) , Heat transfer coefficients , Heat transfer , Thermocouples , Boundary-value problems , Calibration , Convection , Jets
Lateral-Flow Effect on Endwall Heat Transfer and Pressure Drop in a Pin-Fin Trapezoidal Duct of Various Pin Shapes
Jenn-Jiang Hwang, Chau-Ching Lu
GT 2000; V003T01A040https://doi.org/10.1115/2000-GT-0232
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Topics: Ducts , Flow (Dynamics) , Heat transfer , Pressure drop , Shapes , Diamonds , Pins (Engineering) , Reynolds number , Turbulence
Experimental Heat Transfer and Bulk Air Temperature Measurements for a Multipass Internal Cooling Model With Ribs and Bleed
Douglas Thurman, Philip Poinsatte
GT 2000; V003T01A041https://doi.org/10.1115/2000-GT-0233
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Topics: Cooling , Heat transfer , Temperature measurement , Temperature , Strips , Turbine blades , External pressure , Film cooling , Liquid crystals , Steady state
Intercoolers in Gas Turbine Systems and Combi-Processes for Production of Electricity
Arash Saidi, Bengt Sundén, Daniel Eriksson
GT 2000; V003T01A042https://doi.org/10.1115/2000-GT-0234
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Topics: Gas turbines
Influence of Cross-Flow Induced Swirl and Impingement on Heat Transfer in a Two-Pass Channel Connected by Two Rows of Holes
Gautam Pamula, Srinath V. Ekkad, Sumanta Acharya
GT 2000; V003T01A043https://doi.org/10.1115/2000-GT-0235
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Topics: Cross-flow , Heat transfer , Coolants , Channel flow , Cooling , Design , Flow (Dynamics) , Heat transfer coefficients , Liquid crystals , Reynolds number
Effect of Surface Curvature on Heat Transfer and Hydrodynamics Within a Single Hemispherical Dimple
N. Syred, A. Khalatov, A. Kozlov, A. Shchukin, R. Agachev
GT 2000; V003T01A044https://doi.org/10.1115/2000-GT-0236
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Topics: Heat transfer , Hydrodynamics , Vortices , Flow (Dynamics) , Fluid dynamics , Reynolds number , Turbulent heat transfer
Innovative Cyclone Cooling Scheme for Gas Turbine Blade: Thermal-Hydraulic Performance Evaluation
Artem Khalatov, Nick Syred, Philip Bowen, Rashed Al-Ajmi, Alexander Kozlov, Andrey Schukin
GT 2000; V003T01A045https://doi.org/10.1115/2000-GT-0237
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Topics: Blades , Cooling , Gas turbines , Performance evaluation , Heat transfer , Air flow , Compressors , Coolants , Energy dissipation , Flow (Dynamics)
Influence of Injection Type and Feed Arrangement on Flow and Heat Transfer in an Injection Slot
Hyung Hee Cho, Jin Ki Ham
GT 2000; V003T01A046https://doi.org/10.1115/2000-GT-0238
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Topics: Flow (Dynamics) , Heat transfer , Heat , Mass transfer , Coolants , Cooling , Combustion chambers , Computer simulation , Film cooling , Gas turbines
Scaling of Performance for Varying Density Ratio Coolants on an Airfoil With Strong Curvature and Pressure Gradient Effects
Marcia I. Ethridge, J. Michael Cutbirth, David G. Bogard
GT 2000; V003T01A047https://doi.org/10.1115/2000-GT-0239
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Topics: Airfoils , Coolants , Density , Pressure gradient , Film cooling , Turbulence , Flat plates , Momentum , Suction , Temperature distribution
Effects of Showerhead Injection on Film Cooling Effectiveness for a Downstream Row of Holes
Marc D. Polanka, Marcia I. Ethridge, J. Michael Cutbirth, David G. Bogard
GT 2000; V003T01A048https://doi.org/10.1115/2000-GT-0240
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Topics: Film cooling , Coolants , Pressure , Turbulence , Airfoils , Turbines , Boundary layers , Cooling , Density , Flat plates
Novel Blade Cooling Engineering Solution
Siegfried Moser, Mario Ivanisin, Jakob Woisetschläger, Herbert Jericha
GT 2000; V003T01A049https://doi.org/10.1115/2000-GT-0242
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Topics: Blades , Cooling , Turbulence , Computational fluid dynamics , Finite element analysis , Jets , Turbines , Computation , Dimensions , Engineering design
Measurement of Local Heat Transfer Coefficient and Film Cooling Effectiveness Through Discrete Holes
R. F. Martinez-Botas, C. H. N. Yuen
GT 2000; V003T01A050https://doi.org/10.1115/2000-GT-0243
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Topics: Film cooling , Heat transfer coefficients , Density , Liquid crystals , Temperature , Adiabatic cooling , Boundary layers , Cooling , Flat plates , Heat transfer
Effect of Partial Coating Blockage on Film Cooling Effectiveness
Ronald S. Bunker
GT 2000; V003T01A051https://doi.org/10.1115/2000-GT-0244
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Topics: Coatings , Film cooling , Turbines , Airfoils , Coolants , Cross section (Physics) , Databases , Diffusers , Flat plates , Flow (Dynamics)
Transient Liquid Crystal Measurement of Leading Edge Film Cooling Effectiveness and Heat Transfer With High Free Stream Turbulence
Shichuan Ou, Richard Rivir, Matthew Meininger, Fred Soechting, Martin Tabbita
GT 2000; V003T01A052https://doi.org/10.1115/2000-GT-0245
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Topics: Film cooling , Heat transfer , Liquid crystals , Transients (Dynamics) , Turbulence , Reynolds number , Heat transfer coefficients
The Effects of Injection Angle and Hole Exit Shape on Turbine Nozzle Pressure Side Film Cooling
Luzeng J. Zhang, Ram Pudupatty
GT 2000; V003T01A053https://doi.org/10.1115/2000-GT-0247
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Topics: Film cooling , Nozzles , Pressure , Shapes , Turbines , Oxygen , Airfoils , Coolants , Cooling , Flow (Dynamics)
Film Cooling Downstream of a Row of Discrete Holes With Compound Angle
R. J. Goldstein, P. Jin
GT 2000; V003T01A054https://doi.org/10.1115/2000-GT-0248
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Topics: Film cooling , Mass transfer , Density , Heat transfer coefficients , Jets , Vapors , Vortex motion
Reynolds Stress Transport Model Predictions and Large Eddy Simulations for Film Coolant Jet in Crossflow
Asif Hoda, Sumanta Acharya, Mayank Tyagi
GT 2000; V003T01A055https://doi.org/10.1115/2000-GT-0249
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Topics: Coolants , Large eddy simulation , Stress , Flow (Dynamics) , Turbulence , Anisotropy , Approximation , Cooling , Eddies (Fluid dynamics) , Jets
Numerical and Experimental Investigations of the Influence of Different Swirl Ratios on the Temperature Streak Development in a 4-Stage Turbine
Dieter Bohn, Harald Funke, Tom Heuer, Jürg Bütikofer
GT 2000; V003T01A056https://doi.org/10.1115/2000-GT-0250
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Topics: Temperature , Turbines , Cooling , Flow (Dynamics) , Blades , Combustion chambers , Gas turbines
Thermal Conjugate Analysis of a First Stage Blade in a Gas Turbine
Toshihiko Takahashi, Kazunori Watanabe, Takeshi Takahashi
GT 2000; V003T01A057https://doi.org/10.1115/2000-GT-0251
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Topics: Blades , Gas turbines , Temperature , Cooling , Numerical analysis , Air flow , Convection , Heat , Heat conduction , Heat transfer
Local Heat/Mass Transfer Measurement on the Effusion Plate in Impingment/Effusion Cooling System
Hyung Hee Cho, Dong Ho Rhee
GT 2000; V003T01A058https://doi.org/10.1115/2000-GT-0252
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Topics: Cooling systems , Heat , Mass transfer , Plates (structures) , Flow (Dynamics) , Cooling , Jets , Reynolds number , Vortices
Simultaneous Prediction of External Flow-Field and Temperature in Internally Cooled 3-D Turbine Blade Material
Zhen-Xue Han, Brian H. Dennis, George S. Dulikravich
GT 2000; V003T01A059https://doi.org/10.1115/2000-GT-0253
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Topics: Flow (Dynamics) , Temperature , Turbine blades , Convection , Coolants , Heat transfer , Airfoils , Blades , Boundary-value problems , Computers
Heat Transfer Analysis in a Modern DLN Combustor
Giovanni Ferrara, Luca Innocenti, Giacomo Migliorini, Bruno Facchini, Anthony J. Dean
GT 2000; V003T01A060https://doi.org/10.1115/2000-GT-0254
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Topics: Combustion chambers , Heat transfer , Cooling , Emissions , Air flow , Flow (Dynamics) , Fuels , Pressure , Compressors , Convection
Turbulence Structures of Leading Edge Film Cooling Jets
Sabine Ardey, Stefan Wolff, Leonhard Fottner
GT 2000; V003T01A061https://doi.org/10.1115/2000-GT-0255
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Topics: Film cooling , Jets , Turbulence , Pressure , Blades , Suction , Anisotropy , Cascades (Fluid dynamics) , Coolants , Diffusion (Physics)
Flow Characteristics Inside Circular Injection Holes Normally Oriented to a Crossflow: Part I — Flow Visualizations and Flow Data in the Symmetry Plane
Sang Woo Lee, Sang Won Park, Joon Sik Lee
GT 2000; V003T01A062https://doi.org/10.1115/2000-GT-0256
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Topics: Flow (Dynamics) , Flow visualization , Separation (Technology) , Bubbles , Boundary layers , Flow measurement , Visualization
Flow Characteristics Inside Circular Injection Holes Normally Oriented to a Crossflow: Part II — Three Dimensional Flow Data and Aerodynamic Loss
Sang Woo Lee, Seong Kuk Joo, Joon Sik Lee
GT 2000; V003T01A063https://doi.org/10.1115/2000-GT-0257
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Topics: Flow (Dynamics) , Bubbles , Separation (Technology) , Friction
Aerodynamic Loss Characteristics of a Turbine Blade With Trailing Edge Coolant Ejection: Part 1 — Effect of Cut-Back Length, Spanwise Rib Spacing, Free Stream Reynolds Number and Chordwise Rib Length on Discharge Coefficients
Oğuz Uzol, Cengiz Camcı, Boris Glezer
GT 2000; V003T01A064https://doi.org/10.1115/2000-GT-0258
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Topics: Coolants , Discharge coefficient , Reynolds number , Turbine blades , Cooling systems , Flow (Dynamics) , Blades , Fluid mechanics , Fluids , Pressure
Measurements in Separated and Transitional Boundary Layers Under Low-Pressure Turbine Airfoil Conditions
Ralph J. Volino, Lennart S. Hultgren
GT 2000; V003T01A065https://doi.org/10.1115/2000-GT-0260
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Topics: Airfoils , Boundary layers , Pressure , Turbines , Turbulence , Separation (Technology) , Reynolds number , Bubbles , Pressure gradient , Flat plates
High Lift and Aft Loaded Profiles for Low Pressure Turbines
R. J. Howell, O. N. Ramesh, H. P. Hodson, N. W. Harvey, V. Schulte
GT 2000; V003T01A066https://doi.org/10.1115/2000-GT-0261
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Topics: Pressure , Turbines , Wakes , Boundary layers , Blades , Cascades (Fluid dynamics) , Inflow , Engines , Reynolds number , Simulation
Turbine Separation Control Using Pulsed Vortex Generator Jets
Jeffrey P. Bons, Rolf Sondergaard, Richard B. Rivir
GT 2000; V003T01A067https://doi.org/10.1115/2000-GT-0262
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Topics: Generators , Jets , Separation (Technology) , Turbines , Vortices , Blades , Boundary layers , Pressure , Suction , Aircraft engines
Effects of Reynolds Number and Free-Stream Turbulence on Boundary Layer Transition in a Compressor Cascade
Heinz-Adolf Schreiber, Wolfgang Steinert, Bernhard Küsters
GT 2000; V003T01A068https://doi.org/10.1115/2000-GT-0263
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Topics: Boundary layers , Cascades (Fluid dynamics) , Compressors , Reynolds number , Turbulence , Blades , Chords (Trusses) , Airfoils , Bubbles , Coatings
Natural Transition Phenomena on an Axial Compressor Blade
J. D. Hughes, G. J. Walker
GT 2000; V003T01A069https://doi.org/10.1115/2000-GT-0264
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Topics: Blades , Compressors , Waves , Algorithms , Turbulence , Flow (Dynamics) , Inflow , Inlet guide vanes , Probability , Stators
Turbine Blade Entropy Generation Rate: Part I — The Boundary Layer Defined
M. R. D. Davies, F. K. O’Donnell, A. J. Niven
GT 2000; V003T01A070https://doi.org/10.1115/2000-GT-0265
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Topics: Boundary layers , Entropy , Turbine blades , Turbulence , Suction , Blades , Boundary layer turbulence , Cascades (Fluid dynamics) , Computational fluid dynamics , Flow (Dynamics)
Turbine Blade Entropy Generation Rate: Part II — The Measured Loss
F. K. O’Donnell, M. R. D. Davies
GT 2000; V003T01A071https://doi.org/10.1115/2000-GT-0266
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Topics: Entropy , Turbine blades , Turbulence , Boundary layers , Blades , Cascades (Fluid dynamics) , Chords (Trusses) , Laminar flow , Reynolds number , Sensors
Control of Separation Bubble on a Blade Leading Edge by a Stationary Bar Wake
K. Funazaki, Y. Harada, E. Takahashi
GT 2000; V003T01A072https://doi.org/10.1115/2000-GT-0267
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Topics: Blades , Bubbles , Separation (Technology) , Wakes , Boundary layers , Flow (Dynamics) , Flat plates , Flow measurement , Probes , Wire
Comparison of Two Highly Loaded Low Pressure Turbine Cascades Under the Influence of Wake-Induced Transition
Stefan Brunner, Leonhard Fottner, Heinz-Peter Schiffer
GT 2000; V003T01A073https://doi.org/10.1115/2000-GT-0268
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Topics: Pressure , Turbines , Wakes , Cascades (Fluid dynamics) , Flow (Dynamics) , Wind tunnels , Reynolds number , Design , Rotors , Stators
Experimental and Numerical Investigation of Wake-Induced Transition on a Highly Loaded LP Turbine at Low Reynolds Numbers
Peter Stadtmüller, Leonhard Fottner, Andreas Fiala
GT 2000; V003T01A074https://doi.org/10.1115/2000-GT-0269
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Topics: Reynolds number , Turbines , Wakes , Boundary layers , Blades , Pressure , Separation (Technology) , Suction , Cascades (Fluid dynamics) , Generators
Separation Bubbles Under Steady and Periodic-Unsteady Main Flow Conditions
Weiliang Lou, Jean Hourmouziadis
GT 2000; V003T01A075https://doi.org/10.1115/2000-GT-0270
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Topics: Bubbles , Flow (Dynamics) , Separation (Technology) , Pressure , Boundary layers , Oscillations , Reynolds number , Wakes , Blades , Flat plates
The Influence of Multimode Transition Initiated by Periodic Wakes on the Profile Loss of a Linear Compressor Cascade
Reinhold Teusch, Stefan Brunner, Leonhard Fottner, Marius Swoboda
GT 2000; V003T01A076https://doi.org/10.1115/2000-GT-0271
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Topics: Cascades (Fluid dynamics) , Compressors , Wakes , Flow (Dynamics) , Bubbles , Separation (Technology) , Blades , Boundary layers , Reynolds number , Belts
Studies on Turbulence Structure of Boundary Layers Disturbed by Moving Wakes
K. Funazaki, Y. Aoyama
GT 2000; V003T01A077https://doi.org/10.1115/2000-GT-0272
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Topics: Boundary layers , Turbulence , Wakes , Probes , Wire , Flat plates , Fluctuations (Physics) , Sensors , Shear stress
Effects of Turbulence and Solidity on the Boundary Layer Development in a Low Pressure Turbine
W. J. Solomon
GT 2000; V003T01A078https://doi.org/10.1115/2000-GT-0273
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Topics: Boundary layers , Pressure , Turbines , Turbulence , Wakes , Nozzles , Separation (Technology) , Design , Instrumentation , Suction
A Study on Models to Simulate Boundary Layer Transition in Turbomachinery Flows
M. Müller, H. E. Gallus, R. Niehuis
GT 2000; V003T01A079https://doi.org/10.1115/2000-GT-0274
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Topics: Boundary layers , Flow (Dynamics) , Turbomachinery , Modeling , Turbulence , Cascades (Fluid dynamics) , Compressors , Computation , Stability , Steady state
Numerical and Experimental Investigation of Low Reynolds Number Effects on Laminar Flow Separation and Transition in a Cascade of Compressor Blades
Shunji Enomoto, C. Hah, G. V. Hobson
GT 2000; V003T01A080https://doi.org/10.1115/2000-GT-0276
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Topics: Blades , Cascades (Fluid dynamics) , Compressors , Laminar flow , Reynolds number , Separation (Technology) , Flow (Dynamics) , Flow separation , Diffusion (Physics) , Eddies (Fluid dynamics)
Prediction of a Laminar Separation Bubble Over a Controlled-Diffusion Compressor Blade
G. V. Hobson, S. Weber
GT 2000; V003T01A081https://doi.org/10.1115/2000-GT-0277
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Topics: Blades , Bubbles , Compressors , Diffusion (Physics) , Separation (Technology) , Turbulence , Flow (Dynamics) , Cascades (Fluid dynamics) , Algebra , Flow visualization
Bypass Transition Modelling: A New Method Which Accounts for Free-Stream Turbulence Intensity and Length Scale
Paul E. Roach, David H. Brierley
GT 2000; V003T01A082https://doi.org/10.1115/2000-GT-0278
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Topics: Modeling , Turbulence , Boundary layers , Geometry , Pressure gradient , Eddies (Fluid dynamics) , Accounting , Electromagnetic scattering
Droplet Generation by Disintegration of Oil Films at the Rim of a Rotating Disk
A. Glahn, S. Busam, M. F. Blair, K. L. Allard, S. Wittig
GT 2000; V003T01A083https://doi.org/10.1115/2000-GT-0279
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Topics: Drops , Rotating disks , Flow (Dynamics) , Bearings , Aircraft engines , Computational fluid dynamics , Databases , Design , Disks , Trajectories (Physics)
Flow Visualisation in a Rotating Cavity With Axial Throughflow
Dieter E. Bohn, Gregor N. Deutsch, Burkhard Simon, Claus Burkhardt
GT 2000; V003T01A084https://doi.org/10.1115/2000-GT-0280
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Topics: Cavities , Flow visualization , Cooling , Flow (Dynamics) , Heat transfer , Lasers , Reliability , Rotors , Smoke , Stress
Flow and Heat Transfer in a Rotating Cavity With a Stationary Stepped Casing
Abdul A. Jaafar, Fariborz Motallebi, Michael Wilson, J. Michael Owen
GT 2000; V003T01A085https://doi.org/10.1115/2000-GT-0281
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Topics: Cavities , Flow (Dynamics) , Heat transfer , Disks , Computation , Cooling , Turbulence , Cylinders , Gas turbines , Laser Doppler anemometry
Conjugate Heat Transfer Analysis of an Engine Internal Cavity
A. Montenay, L. Paté, J. M. Duboué
GT 2000; V003T01A086https://doi.org/10.1115/2000-GT-0282
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Topics: Cavities , Engines , Heat transfer , Heat conduction , Rotors , Aircraft engines , Blades , Computation , Cooling , Cooling systems
Total Pressure Losses in Rotor Systems With Radial Inflow
D. Brillert, D. Lieser, A. W. Reichert, H. Simon
GT 2000; V003T01A087https://doi.org/10.1115/2000-GT-0283
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Topics: Inflow , Pressure , Rotors , Flow (Dynamics) , Cooling , Compressors , Computational methods , Design , Disks , Engines
Experimental and Numerical Investigation of the Influence of Rotor Blades on Hot Gas Ingestion Into the Upstream Cavity of an Axial Turbine Stage
Dieter Bohn, Bernd Rudzinski, Norbert Sürken, Wolfgang Gärtner
GT 2000; V003T01A088https://doi.org/10.1115/2000-GT-0284
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Topics: Blades , Cavities , Rotors , Turbines , Disks , Sealing (Process) , Stators , Carbon dioxide , Pressure , Annulus
Flow and Heat Transfer in an Industrial Rotor-Stator Rim Sealing Cavity
Alexander V. Mirzamoghadam, Zhenhua Xiao
GT 2000; V003T01A089https://doi.org/10.1115/2000-GT-0285
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Topics: Cavities , Flow (Dynamics) , Heat transfer , Rotors , Sealing (Process) , Stators , Computational fluid dynamics , Disks , Engines , Steady state
Experimental Analysis of the Effect of Swirl on the Pressure Field in Whirling 50% Eccentric Annular Seal
Bernard Robic, Gerald Morrison
GT 2000; V003T01A090https://doi.org/10.1115/2000-GT-0286
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Topics: Experimental analysis , Pressure , Whirls , Reynolds number , Flow (Dynamics) , Stators
Influence of a Honeycomb Facing on the Heat Transfer in a Stepped Labyrinth Seal
K. Willenborg, V. Schramm, S. Kim, S. Wittig
GT 2000; V003T01A091https://doi.org/10.1115/2000-GT-0290
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Topics: Heat transfer , Honeycomb structures , Heat transfer coefficients , Stators , Flow (Dynamics) , Geometry , Engines , Finite element analysis , Jet engines , Pressure
Influence of a Honeycomb Facing on the Flow Through a Stepped Labyrinth Seal
V. Schramm, K. Willenborg, S. Kim, S. Wittig
GT 2000; V003T01A092https://doi.org/10.1115/2000-GT-0291
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Topics: Flow (Dynamics) , Honeycomb structures , Geometry , Stators , Aircraft engines , Turbulence
Computed Effect of Rub-Groove Size on Stepped Labyrinth Seal Performance
David L. Rhode, Richard G. Adams
GT 2000; V003T01A093https://doi.org/10.1115/2000-GT-0292
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Topics: Clearances (Engineering) , Cutting , Friction , Honeycomb structures , Leakage , Navier-Stokes equations , Reynolds number , Turbulence , Wear
Large-Scale Testing to Validate the Influence of External Crossflow on the Discharge Coefficients of Film Cooling Holes
D. A. Rowbury, M. L. G. Oldfield, G. D. Lock
GT 2000; V003T01A094https://doi.org/10.1115/2000-GT-0293
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Topics: Discharge coefficient , Film cooling , Testing , Flow (Dynamics) , Coolants , Pressure , Cascades (Fluid dynamics) , Tunnels , Aircraft engines , Engines
A Method for Correlating the Influence of External Crossflow on the Discharge Coefficients of Film Cooling Holes
D. A. Rowbury, M. L. G. Oldfield, G. D. Lock
GT 2000; V003T01A095https://doi.org/10.1115/2000-GT-0294
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Topics: Discharge coefficient , Film cooling , Engines , Coolants , Mach number , Reynolds number , Cascades (Fluid dynamics) , Flow (Dynamics) , Pressure , Aircraft engines
Systematic Experimental and Numerical Investigations on the Aerothermodynamics of a Film Cooled Turbine Cascade With Variation of the Cooling Hole Shape: Part I — Experimental Approach
Wolfgang Ganzert, Thomas Hildebrandt, Leonhard Fottner
GT 2000; V003T01A096https://doi.org/10.1115/2000-GT-0295
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Topics: Aerodynamics , Cascades (Fluid dynamics) , Cooling , Shapes , Turbines , Heat transfer , Heat transfer coefficients , Film cooling , Pressure , Suction
A Presentation of Detailed Experimental Data of a Suction Side Film Cooled Turbine Cascade
Holger Brandt, Wolfgang Ganzert, Leonhard Fottner
GT 2000; V003T01A097https://doi.org/10.1115/2000-GT-0296
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Topics: Cascades (Fluid dynamics) , Suction , Turbines , Heat transfer , Flow (Dynamics) , Steady state , Aerodynamics , Boundary layers , Film cooling , Gas turbines
Film Cooling Jet Aerodynamics for a Pipe and a Converging Nozzle Injection Hole
Jun Sasahara, Yukiko Suzuki, Shigeru Tanaka, Takaaki Shizawa, Shinji Honami
GT 2000; V003T01A098https://doi.org/10.1115/2000-GT-0297
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Topics: Aerodynamics , Film cooling , Nozzles , Pipes , Flow (Dynamics) , Boundary layer turbulence , Cooling , Flat plates , Kidney , Kinetic energy
Systematic Experimental and Numerical Investigations on the Aerothermodynamics of a Film Cooled Turbine Cascade With Variation of the Cooling Hole Shape: Part II — Numerical Approach
Thomas Hildebrandt, Wolfgang Ganzert, Leonhard Fottner
GT 2000; V003T01A099https://doi.org/10.1115/2000-GT-0298
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Topics: Aerodynamics , Cascades (Fluid dynamics) , Cooling , Shapes , Turbines , Flow (Dynamics) , Computational fluid dynamics , Resolution (Optics) , Engineering simulation , Film cooling
Effects of Gap Leakage on Fluid Flow in a Contoured Turbine Nozzle Guide Vane
Y.-L. Lin, T. I-P. Shih, M. K. Chyu, R. S. Bunker
GT 2000; V003T01A100https://doi.org/10.1115/2000-GT-0555
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Topics: Fluid dynamics , Leakage , Nozzle guide vanes , Turbines , Airfoils , Flow (Dynamics) , Computation , Finite volume methods , Momentum , Nozzles
Control of Secondary Flows in a Turbine Nozzle Guide Vane by Endwall Contouring
T. I-P. Shih, Y.-L. Lin, T. W. Simon
GT 2000; V003T01A101https://doi.org/10.1115/2000-GT-0556
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Topics: Flow (Dynamics) , Nozzle guide vanes , Turbines , Airfoils , Film cooling , Computation , Finite volume methods , Momentum , Reynolds number , Shear stress
Aerodynamic Loss Characteristics of a Turbine Blade With Trailing Edge Coolant Ejection: Part 2 — External Aerodynamics, Total Pressure Losses and Predictions
Oğuz Uzol, Cengiz Camcı
GT 2000; V003T01A102https://doi.org/10.1115/2000-GT-0557
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Topics: Aerodynamics , Coolants , Pressure , Turbine blades , Wakes , Blades , Flow (Dynamics) , Turbulence , Algebra , Computer simulation
Measurements in Film Cooling With Lateral Injection: Adiabatic Effectiveness Values and Temperature Fields
Rohit A. Oke, Terrence W. Simon
GT 2000; V003T01A103https://doi.org/10.1115/2000-GT-0597
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Topics: Film cooling , Temperature , Jets , Flow (Dynamics) , Momentum , Probes , Thermocouples
Detailed Flow and Heat Transfer Coefficient Measurements in a Model of an Internal Cooling Geometry Employing Orthogonal Intersecting Channels
David R. H. Gillespie, Peter T. Ireland, Geoff M. Dailey
GT 2000; V003T01A104https://doi.org/10.1115/2000-GT-0653
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Topics: Cooling , Flow (Dynamics) , Geometry , Heat transfer coefficients , Engines , Reynolds number , Temperature , Airfoils , Film cooling , Gas turbines

Electric Power

Developing the Next Generation Gas Turbine Systems — A National Partnership
A. W. Layne
GT 2000; V003T02A001https://doi.org/10.1115/2000-GT-0176
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Topics: Gas turbines , Turbines , Industrial research , Energy efficiency , Energy generation , Governments , Renewable energy , Workshops (Work spaces)
Managing Fuel Oil Nozzle Coking to Improve Gas Turbine Availability
Leo R. Burgett, Tim Mercer
GT 2000; V003T02A002https://doi.org/10.1115/2000-GT-0177
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Topics: Fuel management , Gas turbines , Nozzles , Fuel oils , Cooling , Power stations , Engines , Fuels , Inspection , Motors
Hot-Gas-Path Life Extension Options for the V94.2 Gas Turbine
Gerhard Bohrenkämper, Herbert Bals, Ursel Wrede, René Umlauft
GT 2000; V003T02A003https://doi.org/10.1115/2000-GT-0178
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Topics: Gas turbines , Life extension , Service life (Equipment) , Combined cycle power stations , Maintenance , Power stations , Stress
Early Detection of Combustor Pulsations and Optimized Operation Through On-Line Monitoring Systems
Helmer Andersen
GT 2000; V003T02A004https://doi.org/10.1115/2000-GT-0180
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Topics: Combustion chambers , Monitoring systems , Failure , Maintenance , Combustion systems , Equipment performance , Firing , Gas turbines , Heat , Nitrogen oxides
Power Plants Up-Rating Benefit From Technology Advancements: A Case Study
Robert McCue, Axel W. von Rappard
GT 2000; V003T02A005https://doi.org/10.1115/2000-GT-0181
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Topics: Power stations , Maintainability , Reliability , Heat , Combined cycle power stations , Cycles , Engines , Failure , Gas turbines
Integration of a Gas Turbine (GT) With a Compressed Air Storage (CAES) Plant Provides the Best Alternative for Mid-Range and Daily Cyclic Generation Needs
Michael Nakhamkin, Septimus van der Linden
GT 2000; V003T02A006https://doi.org/10.1115/2000-GT-0182
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Topics: Compressed air , Gas turbines , Storage , Cycles , Power stations , Combustion , Emissions , Energy generation , Energy storage , Fuel consumption
Life Extension of GT HGP Components by Recycling
Jung-Ho Lee
GT 2000; V003T02A007https://doi.org/10.1115/2000-GT-0184
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Topics: Life extension , Recycling , Maintenance , Economic analysis , Gas turbines , Turbine blades
A Neural Network Simulator of a Gas Turbine With a Waste Heat Recovery Section
C. Boccaletti, G. Cerri, B. Seyedan
GT 2000; V003T02A008https://doi.org/10.1115/2000-GT-0185
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Topics: Artificial neural networks , Gas turbines , Heat recovery , Algorithms , Boilers , Feedforward control , Instrumentation , Optimization , Power stations , Steady state
Manufacturers’ Role in the Power Industry
Dilip K. Mukherjee
GT 2000; V003T02A009https://doi.org/10.1115/2000-GT-0186
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Topics: Energy industry , Economics
Development of a Maintenance Program for Major Gas Turbine Hot Gas Path Parts
Hideto Moritsuka, Tomoharu Fujii, Takeshi Takahashi
GT 2000; V003T02A010https://doi.org/10.1115/2000-GT-0187
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Topics: Gas turbines , Maintenance , Turbines , Combined cycle power stations , Temperature , Combined cycles , Combustion chambers , Electricity (Physics) , Energy generation , Nozzles
Risk-Based Inspection of Combustion Turbines
Michael E. G. Schmidt, David A. Mauney
GT 2000; V003T02A011https://doi.org/10.1115/2000-GT-0189
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Topics: Combustion , Risk-based inspection , Turbines , Reliability , Maintenance , Risk , Algorithms , Inspection , Machinery , Mechanical engineers
World’s First LM5000 to LM6000 Cogeneration Plant Repowering
Michael T. McCarrick, Robert K. Rosencrance
GT 2000; V003T02A012https://doi.org/10.1115/2000-GT-0190
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Topics: Cogeneration plants , Gas turbines , Heat , Heat recovery steam generators , Dimensions , Emissions , Exhaust systems , Flow (Dynamics) , Reliability , Temperature
Combustion Turbine Inlet Conditioning: A State-of-the-Art Method of Increasing Generating Capacity Without the Addition of New Basic Generation Hardware
Lloyd B. Tisdale, Robert L. Hauck
GT 2000; V003T02A013https://doi.org/10.1115/2000-GT-0192
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Topics: Combustion , Design , Engineers , Hardware , Turbines
Modular Uprating and Upgrading Solutions in ABB ALSTOM POWER Gas Turbines
Wilfried De Backer, Carsten Bopp
GT 2000; V003T02A014https://doi.org/10.1115/2000-GT-0306
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Topics: Gas turbines
What is the Electric Output of a Cogeneration Project Worth?
Alexandra C. de Kok, Jane P. Hill
GT 2000; V003T02A015https://doi.org/10.1115/2000-GT-0589
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Topics: Combined heat and power , Economics
Kalaeloa — Combined Cycle Power Station Burning LSFO in its Ninth Successful Year
Ziad R. Khalaf, Benno Basler
GT 2000; V003T02A016https://doi.org/10.1115/2000-GT-0590
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Topics: Combined cycle power stations , Combustion , Cogeneration plants , Firing , Power stations , Turbines
Experience With a Fast Track Power Generation Project
Albrecht H. Mayer, Noel W. Lively
GT 2000; V003T02A017https://doi.org/10.1115/2000-GT-0591
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Topics: Combined cycles , Conceptual design , Construction , Cycles , Design , Energy generation , Evaporative cooling , Feedback , Gas turbines , Plant design
Dynamic Behaviour of a Vertical Natural Circulation Two Pressure Stage HRSG Behind a Heavy Duty Gas Turbine
Georg N. Stamatelopoulos, Karl Ponweiser, Heimo Walter, Wladimir Linzer, Hubert Neßler, Robert Strohmaier
GT 2000; V003T02A018https://doi.org/10.1115/2000-GT-0592
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Topics: Gas turbines , Heat recovery steam generators , Pressure , Design , Reliability , Stress , Combined cycle gas turbines , Optimization , Simulation , Temperature
A Recuperated Gas Turbine Incorporating External Heat Sources in the Combined Gas-Steam Cycle
Ryszard Chodkiewicz, Jan Krysinski, Jerzy Porochnicki
GT 2000; V003T02A019https://doi.org/10.1115/2000-GT-0593
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Topics: Cycles , Gas turbines , Heat , Steam , Exhaust systems , Gases , Air pollution , Compressed air , Electricity (Physics) , Turbines
The Single-Shaft Combined Cycle Myth
Ram G. Narula
GT 2000; V003T02A020https://doi.org/10.1115/2000-GT-0594
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Topics: Combined cycle power stations , Combined cycles , Energy generation , Gas turbines , Performance , Power stations , Thermal efficiency , Trains
Alabama Electric Cooperative Compressed Air Energy Storage (CAES) Plant Improvements
Paul Holden, David Moen, Mario DeCorso, John Howard
GT 2000; V003T02A021https://doi.org/10.1115/2000-GT-0595
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Topics: Combustion chambers , Compressed air , Durability , Emissions , Energy storage , Fuel injectors , Instrumentation , Maintenance , Metals , Reliability
Injecting Humidified and Heated Air to Meet Peak Power Demands
Michael Nakhamkin, Ronald Wolk, Boris Potashnik, Thomas Butler, Ronald Hall
GT 2000; V003T02A022https://doi.org/10.1115/2000-GT-0596
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Topics: Combustion , Combustion chambers , Energy storage , Gas turbines , Heat , Power stations , Temperature , Turbines
Use of Unconventional Fuels in Gas Turbines
Dilip K. Mukherjee
GT 2000; V003T02A023https://doi.org/10.1115/2000-GT-0637
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Topics: Fuels , Gas turbines , Combustion , Condensed matter , Design , Blast furnaces , China , Combined cycle power stations , Combined cycles , Combustion chambers

Industrial and Cogeneration

Strategy for a Cost Optimized Operation of a Flexible Cogeneration Gas Turbine Plant
D. Hein, K. Kwanka, M. Nixdorf
GT 2000; V003T03A001https://doi.org/10.1115/2000-GT-0299
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Topics: Combined heat and power , Gas turbines , Cycles , Cogeneration plants , Heat
Spinning Reserve Influence in a Power Generating System Integrated by Hydro Storage Plants
M. Bianchi, E. Gadda, A. Peretto
GT 2000; V003T03A002https://doi.org/10.1115/2000-GT-0300
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Topics: Spin (Aerodynamics) , Spinning (Textile) , Storage , Stress , Energy / power systems , Fossil fuels , Energy consumption , Fuel consumption , Fuels , Power stations
Selection of Cycle Configurations for Combined Cycle Cogeneration Power Plants
Rattan Tawney, John Ehman, Mona Brown
GT 2000; V003T03A003https://doi.org/10.1115/2000-GT-0301
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Topics: Cogeneration plants , Combined cycles , Cycles , Steam , Economics , Energy generation , Flow (Dynamics) , Combined heat and power , Energy industry , Gas turbines
PEACES: A Program for the Economic Analysis of Combined Energy Systems
Joseph Roy-Aikins
GT 2000; V003T03A004https://doi.org/10.1115/2000-GT-0302
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Topics: Economic analysis , Energy / power systems , Computer software , Combined cycles , Combined heat and power , Economics , Life cycle costing , Steam turbines , Waste heat
Application of Evaporative Coolers for Gas Turbine Power Plants
J. Douglas McNeilly
GT 2000; V003T03A005https://doi.org/10.1115/2000-GT-0303
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Topics: Coolers , Gas turbines , Power stations , Temperature , Water , Compressors , Drops , Evaporation , High temperature , Plasma spraying
Evaluation of Operational Performance of a Gas Turbine Cogeneration Plant With Intake Air Cooled by Ice Storage
Ryohei Yokoyama, Koichi Ito
GT 2000; V003T03A006https://doi.org/10.1115/2000-GT-0304
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Topics: Cogeneration plants , Gas turbines , Ice , Storage , Cooling , Central heating , Compression , Linear programming , Temperature
Fog System Performance in Power Augmentation of Heavy Duty Power Generating Gas Turbines Model 7EA
Steve Ingistov
GT 2000; V003T03A007https://doi.org/10.1115/2000-GT-0305
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Topics: Gas turbines , Water , Compressors , Particulate matter , Compression , Evaporation , Information Analysis Centers , Inlet guide vanes , Machinery , Pressure
Inlet Fogging of Gas Turbine Engines: Part A — Theory, Psychrometrics and Fog Generation
Cyrus B. Meher-Homji, Thomas R. Mee, III
GT 2000; V003T03A008https://doi.org/10.1115/2000-GT-0307
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Topics: Gas turbines , Temperature , Evaporative cooling , Mechanical drives , Petrochemicals , Process industries , Public utilities
Inlet Fogging of Gas Turbine Engines: Part B — Practical Considerations, Control, and O&M Aspects
Cyrus B. Meher-Homji, Thomas R. Mee, III
GT 2000; V003T03A009https://doi.org/10.1115/2000-GT-0308
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Topics: Gas turbines , Compressors , Cooling , Design , Evaporative cooling , Maintenance , Nozzles , Temperature , Water pollution
Set-Up of an Adaptive Method for the Diagnosis of Gas Turbine Operating State by Using Test-Bench Measurements
R. Bettocchi, P. R. Spina, E. Benvenuti
GT 2000; V003T03A010https://doi.org/10.1115/2000-GT-0309
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Topics: Gas turbines , Cycles , Instrumentation , Machinery
Optimum Management System With Environmental Monitoring
G. Cerri, R. Evans, C. A. Frangopoulos, M. Parrella, R. U. Pitt, J. Psychogios, S. Salvador, M. Sepielli, B. Seyedan
GT 2000; V003T03A011https://doi.org/10.1115/2000-GT-0310
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Topics: Boundary-value problems , Calibration , Cogeneration plants , Computer software , Computers , Engineering prototypes , Optimization , Stress
Gas Turbine Field Performance Determination: Sources of Uncertainties
M. Pinelli, P. R. Spina
GT 2000; V003T03A012https://doi.org/10.1115/2000-GT-0311
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Topics: Gas turbines , Uncertainty , Errors , Thermodynamic cycles
Real-Time On-Line Performance Diagnostics of Heavy-Duty Industrial Gas Turbines
S. Can Gülen, Patrick R. Griffin, Sal Paolucci
GT 2000; V003T03A013https://doi.org/10.1115/2000-GT-0312
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Topics: Cogeneration plants , Combined cycles , Compressors , Computer software , Control systems , Databases , Engines , Filters , Gas turbines , Industrial gases
Influence of Ambient Conditions on an Aeroderivative Gas Turbine Based Cogeneration Plant — A Comparison of Numerical Simulation With Field Performance Data
Carlo Carcasci, Bruno Facchini, Francesco Grillo
GT 2000; V003T03A014https://doi.org/10.1115/2000-GT-0313
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Topics: Cogeneration plants , Computer simulation , Gas turbines , Design , Power stations , Temperature , Boundary-value problems , Combined heat and power , Compressors , Cooling systems
Remote Monitoring and Diagnostics System for GE Heavy Duty Gas Turbines
Dincer Ozgur, Arkalgud N. Lakshminarasimha, Richard Rucigay, Mahesh Morjaria, S. Sanborn
GT 2000; V003T03A015https://doi.org/10.1115/2000-GT-0314
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Topics: Gas turbines , Design , Algorithms , Combustion , Computers , Energy generation , Maintenance , Power stations , Turbines , Vibration
Inverted Brayton Cycle Employment for Low Temperature Cogenerative Applications
M. Bianchi, G. Negri di Montenegro, A. Peretto
GT 2000; V003T03A016https://doi.org/10.1115/2000-GT-0315
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Topics: Brayton cycle , Low temperature , Cogeneration plants , Gas turbines , Diesel , Electricity (Physics) , Gasoline engines , Power stations
Thermo-Economic Analysis of an Intercooled, Reheat and Recuperated Gas Turbine for Cogeneration Applications: Part I — Base Load Operation
R. Bhargava, M. Bianchi, G. Negri di Montenegro, A. Peretto
GT 2000; V003T03A017https://doi.org/10.1115/2000-GT-0316
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Topics: Combined heat and power , Gas turbines , Stress , Thermoeconomics , Cycles , Pressure , Compressors , Economic analysis , Heat , Heat recovery
Utilization of Cryogenic Exergy of LNG by MGT (Mirror Gas Turbine)
Y. Tsujikawa, K. Kaneko, S. Fujii
GT 2000; V003T03A018https://doi.org/10.1115/2000-GT-0317
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Topics: Exergy , Gas turbines , Liquefied natural gas , Mirrors , Cycles , Seawater , Brayton cycle , Climate change , Combined cycles , Evaporation
Performance Prediction of Small-Scale Tri-Generation Plants Based on Integrated SOFC and Microturbine Systems
Stefano Campanari, Ennio Macchi
GT 2000; V003T03A019https://doi.org/10.1115/2000-GT-0318
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Topics: Microturbines , Solid oxide fuel cells , Absorption , Carbon dioxide , Commercial construction , Compression , Cooling , Economic analysis , Electric power generation , Electricity (Physics)
Evaluation of Cyclic Operation of Heat Recovery Steam Generators — A Practical Approach
Lewis R. Douglas, Joseph E. Schroeder, Vernon L. Eriksen
GT 2000; V003T03A020https://doi.org/10.1115/2000-GT-0319
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Topics: Heat recovery steam generators , Cycles , Damage , Fatigue , Generators , Heat , High cycle fatigue , Power stations
A Steady State Calculation Model for Gas Turbine Thermal Enclosures
Umberto Desideri, Francesco Di Maria
GT 2000; V003T03A021https://doi.org/10.1115/2000-GT-0320
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Topics: Gas turbines , Steady state , Cooling systems , Fire , Heat , Mechanical drives , Pipes , Temperature , Acoustics , Compression
Brush Seals for the No. 3 Bearing of a Model 7EA Gas Turbine
Steve Ingistov, Gary Meredith, Erik Sulda
GT 2000; V003T03A022https://doi.org/10.1115/2000-GT-0558
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Topics: Bearings , Gas turbines , Rotors , Leakage , Cavities , Compressors , Polishing equipment , High pressure (Physics) , Journal bearings , Lubricating oils
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