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Proceedings Papers
Volume 3: Heat Transfer; Electric Power; Industrial and Cogeneration
Heat Transfer
Numerical Study of Hot Gas Ingestion Into an Engine Type High-Pressure Turbine Rotor-Stator Cavity
GT 2001; V003T01A001https://doi.org/10.1115/2001-GT-0114
Topics:
Cavities
,
Engines
,
High pressure (Physics)
,
Rotors
,
Stators
,
Turbines
,
Flow (Dynamics)
,
Pressure
,
Sealing (Process)
,
Temperature
Droplet Entrainment From a Shear-Driven Liquid Wall Film in Inclined Ducts: Experimental Study and Correlation Comparison
GT 2001; V003T01A002https://doi.org/10.1115/2001-GT-0115
Topics:
Drops
,
Ducts
,
Shear (Mechanics)
,
Flow (Dynamics)
,
Chemical engineering
,
Databases
,
Film flow
,
Film thickness
,
Gas flow
,
Liquid films
An Experimental Study of Liquid Film Thickness in Annular Air/Oil Flow in a Vertical Pipe Using a Laser Focus Displacement Meter
GT 2001; V003T01A003https://doi.org/10.1115/2001-GT-0116
Topics:
Displacement
,
Flow (Dynamics)
,
Lasers
,
Liquid films
,
Pipes
,
Bearings
,
Engines
,
Film thickness
,
Pressure
,
Temperature
Predicted Effects of Bearing Sump and Injection Pressures on Oil Labyrinth Leakage
GT 2001; V003T01A005https://doi.org/10.1115/2001-GT-0118
Topics:
Bearings
,
Leakage
,
Vapors
,
Flow (Dynamics)
,
Polishing equipment
,
Pressure
,
Computers
Mainstream Aerodynamic Effects due to Wheelspace Coolant Injection in a High-Pressure Turbine Stage: Part I — Aerodynamic Measurements in the Stationary Frame
GT 2001; V003T01A006https://doi.org/10.1115/2001-GT-0119
Topics:
Coolants
,
High pressure (Physics)
,
Turbines
,
Cooling
,
Rotors
,
Axial flow
,
Boundary layers
,
Cavities
,
Flow (Dynamics)
,
Impingement cooling
Mainstream Aerodynamic Effects due to Wheelspace Coolant Injection in a High-Pressure Turbine Stage: Part II — Aerodynamic Measurements in the Rotational Frame
GT 2001; V003T01A007https://doi.org/10.1115/2001-GT-0120
Topics:
Coolants
,
High pressure (Physics)
,
Turbines
,
Cooling
,
Flow (Dynamics)
,
Rotors
,
Nozzle guide vanes
,
Axial flow
,
Boundary layers
,
Impingement cooling
A Converging Slot-Hole Film-Cooling Geometry: Part 1 — Low-Speed Flat-Plate Heat Transfer and Loss
GT 2001; V003T01A012https://doi.org/10.1115/2001-GT-0126
Topics:
Film cooling
,
Flat plates
,
Geometry
,
Heat transfer
,
Engines
,
Heat flux
,
Temperature
,
Adiabatic cooling
,
Blades
,
Boundary layers
A Converging Slot-Hole Film-Cooling Geometry: Part 2 — Transonic Nozzle Guide Vane Heat Transfer and Loss
GT 2001; V003T01A013https://doi.org/10.1115/2001-GT-0127
Topics:
Film cooling
,
Geometry
,
Heat transfer
,
Nozzle guide vanes
,
Engines
,
Coolants
,
Tunnels
,
Adiabatic cooling
,
Blades
,
Computers
Effects of Bulk Flow Pulsations on Film Cooling With Compound Angle Holes: Heat Transfer Coefficient Ratio and Heat Flux Ratio
GT 2001; V003T01A015https://doi.org/10.1115/2001-GT-0129
Topics:
Film cooling
,
Flow (Dynamics)
,
Heat flux
,
Heat transfer coefficients
,
Coolants
,
Blades
,
Liquid crystals
,
Pressure
,
Temperature
,
Wind tunnels
Full-Coverage Film Cooling With Short Normal Injection Holes
GT 2001; V003T01A016https://doi.org/10.1115/2001-GT-0130
Topics:
Film cooling
,
Coolants
,
Turbulence
,
Flat plates
,
Density
,
Engines
,
Infrared imaging
,
Jets
,
Resolution (Optics)
,
Separation (Technology)
Film Cooling Effectiveness Downstream of Compound and Fan-Shaped Holes
GT 2001; V003T01A017https://doi.org/10.1115/2001-GT-0131
Topics:
Film cooling
,
Fluids
,
Momentum
,
Shapes
,
Carbon dioxide
,
Cooling
,
Density
,
Flat plates
,
Flow (Dynamics)
,
Heat transfer coefficients
Comparison of Cooling Film Development Calculations for Transpiration Cooled Flat Plates With Different Turbulence Models
GT 2001; V003T01A018https://doi.org/10.1115/2001-GT-0132
Topics:
Cooling
,
Flat plates
,
Transpiration
,
Turbulence
,
Flow (Dynamics)
,
Fluid dynamics
,
Thermal barrier coatings
,
Combustion chambers
,
Coolants
,
Gas turbines
Shock Wave - Film Cooling Interactions in Transonic Flows
GT 2001; V003T01A019https://doi.org/10.1115/2001-GT-0133
Topics:
Film cooling
,
Shock waves
,
Transonic flow
,
Mach number
,
Cross-flow
,
Coolants
,
Cooling
,
Density
,
Flow separation
,
Shock (Mechanics)
Boundary Layer and Loss Analysis in a Film Cooled Vane
GT 2001; V003T01A022https://doi.org/10.1115/2001-GT-0136
Topics:
Boundary layers
,
Coolants
,
Pressure
,
Suction
,
Wakes
,
Blades
,
Cascades (Fluid dynamics)
,
Chords (Trusses)
,
Cooling
,
Flow (Dynamics)
Coarse Grid Modeling of Turbine Film Cooling Flows Using Volumetric Source Terms
GT 2001; V003T01A023https://doi.org/10.1115/2001-GT-0138
Topics:
Film cooling
,
Flow (Dynamics)
,
Modeling
,
Turbines
,
Design
,
Computation
,
Boundary layers
,
Computer simulation
,
Cycles
,
Density
Influence of Freestream Turbulence Intensity on Cooling Effectiveness
GT 2001; V003T01A024https://doi.org/10.1115/2001-GT-0139
Topics:
Cooling
,
Turbulence
,
Computation
,
Algebra
,
Anisotropy
,
Boundary layers
,
Flow (Dynamics)
,
Geometry
,
Heat transfer
,
Reynolds number
Numerical Prediction of Combustor Heatshield Flow and Heat Transfer With Sub-Grid-Scale Modelling of Pedestals
GT 2001; V003T01A027https://doi.org/10.1115/2001-GT-0144
Topics:
Combustion chambers
,
Flow (Dynamics)
,
Heat transfer
,
Modeling
,
Temperature
,
Ducts
,
Fluids
,
Friction
,
Geometry
,
Momentum
Film-Cooled Turbine Endwall in a Transonic Flow Field: Part I — Aerodynamic Measurements
GT 2001; V003T01A028https://doi.org/10.1115/2001-GT-0145
Topics:
Transonic flow
,
Turbines
,
Coolants
,
Flow (Dynamics)
,
Pressure
,
Cascades (Fluid dynamics)
,
Film cooling
,
Convection
,
Engines
,
Flow visualization
Film-Cooled Turbine Endwall in a Transonic Flow Field: Part II — Heat Transfer and Film-Cooling Effectiveness
GT 2001; V003T01A029https://doi.org/10.1115/2001-GT-0146
Topics:
Film cooling
,
Heat transfer
,
Transonic flow
,
Turbines
,
Coolants
,
Flow (Dynamics)
,
Cascades (Fluid dynamics)
,
Cooling
,
Design
,
Engines
Turbine Nozzle Endwall Film Cooling Study Using Pressure Sensitive Paint
GT 2001; V003T01A030https://doi.org/10.1115/2001-GT-0147
Topics:
Film cooling
,
Nozzles
,
Paints
,
Pressure
,
Turbines
,
Flow (Dynamics)
,
Cooling
,
Cascades (Fluid dynamics)
,
Jets
,
Mach number
Mist/Steam Cooling by a Row of Impinging Jets
GT 2001; V003T01A034https://doi.org/10.1115/2001-GT-0151
Topics:
Cooling
,
Jets
,
Steam
,
Drops
,
Flow (Dynamics)
,
Heat transfer coefficients
,
Airfoils
,
Computational fluid dynamics
,
Heat flux
,
Reynolds number
Prediction of Relaminarization Effects on Turbine Blade Heat Transfer
GT 2001; V003T01A041https://doi.org/10.1115/2001-GT-0162
Topics:
Heat transfer
,
Turbine blades
,
Rotors
,
Blades
,
Reynolds number
,
Turbulence
,
Pressure
,
Pressure gradient
,
Accounting
,
Cooling
The Many Faces of Turbine Surface Roughness
GT 2001; V003T01A042https://doi.org/10.1115/2001-GT-0163
Topics:
Surface roughness
,
Turbines
,
Coating processes
,
Coatings
,
Computation
,
Erosion
,
Film cooling
,
Pressure
,
Spallation (Nuclear physics)
,
Suction
Measurements in a Turbine Cascade Flow Under Ultra Low Reynolds Number Conditions
Kenneth W. Van Treuren, Terrence Simon, Marc von Koller, Aaron R. Byerley, James W. Baughn, Richard Rivir
GT 2001; V003T01A043https://doi.org/10.1115/2001-GT-0164
Topics:
Flow (Dynamics)
,
Reynolds number
,
Turbines
,
Suction
,
Separation (Technology)
,
Turbulence
,
Vortices
,
Generators
,
Gas turbines
,
Pressure
Analysis of the Influence of Cooling Steam Conditions on the Cooling Efficiency of a Steam-Cooled Vane Using the Conjugate Calculation Technique
GT 2001; V003T01A045https://doi.org/10.1115/2001-GT-0166
Topics:
Cooling
,
Steam
,
Temperature
,
Pressure
,
Blades
,
Cascades (Fluid dynamics)
,
Compressors
,
Convection
,
Flow (Dynamics)
,
Gas turbines
Turbulence and Vorticity Effects on Stagnation Region Heat Transfer
GT 2001; V003T01A046https://doi.org/10.1115/2001-GT-0168
Topics:
Heat transfer
,
Turbulence
,
Vorticity
,
Rods
,
Reynolds number
,
Vortices
,
Wind tunnels
Detailed Boundary Layer Measurements on a Turbine Stator Vane at Elevated Freestream Turbulence Levels
GT 2001; V003T01A047https://doi.org/10.1115/2001-GT-0169
Topics:
Boundary layers
,
Stators
,
Turbines
,
Turbulence
,
Airfoils
,
Pressure
,
Suction
,
Combustion chambers
,
Fluctuations (Physics)
,
Gas turbines
Flow Field Simulations of a Gas Turbine Combustor
GT 2001; V003T01A048https://doi.org/10.1115/2001-GT-0170
Topics:
Combustion chambers
,
Flow (Dynamics)
,
Gas turbines
,
Simulation
,
Turbines
,
Jets
,
Nozzle guide vanes
,
Boundary layer turbulence
,
Cooling
,
Pressure
Transient Analyses of Conjugate Heat Transfer of a First Stage Rotor Blade in Start-Up and Shut-Down
GT 2001; V003T01A049https://doi.org/10.1115/2001-GT-0171
Topics:
Blades
,
Heat transfer
,
Rotors
,
Transient analysis
,
Stress
,
Heat conduction
,
Temperature
,
Convection
,
Creep
,
Energy generation
Heat Transfer Computations for High Pressure Turbines
GT 2001; V003T01A050https://doi.org/10.1115/2001-GT-0172
Topics:
Computation
,
Heat transfer
,
High pressure (Physics)
,
Turbines
,
Blades
,
Airfoils
,
Cooling systems
,
Design
,
Engines
,
High temperature
Study of Hot Streak Effects in a Counter-Rotating Turbine
GT 2001; V003T01A051https://doi.org/10.1115/2001-GT-0173
Topics:
Turbines
,
Blades
,
Heat
,
Stress
,
Convection
,
Design
,
Flow (Dynamics)
,
High pressure (Physics)
,
Optimization
,
Pressure
Steady Three-Dimensional Simulation of a Transonic Axial Turbine Stage
GT 2001; V003T01A052https://doi.org/10.1115/2001-GT-0174
Topics:
Simulation
,
Turbines
,
Pressure
,
Stators
,
Blades
,
Computation
,
Computational fluid dynamics
,
Coolants
,
Leakage
,
Reynolds number
Heat Transfer Characteristics of a Flow Passage With Long Pin Fins and Improving Heat Transfer Coefficient by Adding Turbulence Promoters on a Endwall
GT 2001; V003T01A054https://doi.org/10.1115/2001-GT-0178
Topics:
Fins
,
Flow (Dynamics)
,
Heat transfer
,
Heat transfer coefficients
,
Turbulence
,
Turbines
,
Blades
,
Cooling
,
Thermal conductivity
,
Airfoils
Integration of Multi-Disciplinary Factors Into Turbine Cooling Design
GT 2001; V003T01A055https://doi.org/10.1115/2001-GT-0179
Topics:
Cooling
,
Design
,
Turbines
,
Blades
,
Engineering disciplines
,
Combustion chambers
,
Disks
,
Engines
,
Gas turbines
,
Nozzles
Elliptical Pin Fins as an Alternative to Circular Pin Fins for Gas Turbine Blade Cooling Applications: Part 1 — Endwall Heat Transfer and Total Pressure Loss Characteristics
GT 2001; V003T01A056https://doi.org/10.1115/2001-GT-0180
Topics:
Blades
,
Cooling
,
Fins
,
Gas turbines
,
Heat transfer
,
Pressure
,
Convection
,
Flow (Dynamics)
,
Liquid crystals
,
Reynolds number
Elliptical Pin Fins as an Alternative to Circular Pin Fins for Gas Turbine Blade Cooling Applications: Part 2 — Wake Flow Field Measurements and Visualization Using Particle Image Velocimetry
GT 2001; V003T01A057https://doi.org/10.1115/2001-GT-0181
Topics:
Blades
,
Cooling
,
Fins
,
Gas turbines
,
Particulate matter
,
Visualization
,
Wakes
,
Flow (Dynamics)
,
Momentum
,
Turbulence
Quasi Two-Dimensional Cyclone-Jet Cooling Configuration: Evaluation of Heat Transfer and Pressure Losses
GT 2001; V003T01A058https://doi.org/10.1115/2001-GT-0182
Topics:
Cooling
,
Heat transfer
,
Pressure
,
Flow (Dynamics)
,
Heat flux
,
Thermal efficiency
,
Boundary-value problems
,
Design
,
Flow separation
,
Heating
Effect of Rib Turbulators in the First Pass on Heat Transfer Distributions in a Two-Pass Channel Connected by Two Rows of Holes
GT 2001; V003T01A059https://doi.org/10.1115/2001-GT-0184
Topics:
Heat transfer
,
Coolants
,
Cooling
,
Flow (Dynamics)
,
Reynolds number
,
Blades
,
Gas turbines
,
Heat transfer coefficients
The Fluid Dynamics of LPT Blade Separation Control Using Pulsed Jets
GT 2001; V003T01A064https://doi.org/10.1115/2001-GT-0190
Topics:
Blades
,
Fluid dynamics
,
Jets
,
Separation (Technology)
,
Boundary layers
,
Cycles
,
Vortices
,
Generators
,
Relaxation (Physics)
,
Turbines
Measurements of the Effects of Pressure-Gradient History on Separation-Bubble Transition
GT 2001; V003T01A067https://doi.org/10.1115/2001-GT-0193
Topics:
Bubbles
,
Pressure gradient
,
Separation (Technology)
,
Boundary layers
,
Chords (Trusses)
,
Turbulence
,
Blades
,
Flat plates
,
Reynolds number
,
Turbomachinery
On the Impact of Blade Count Reduction on Aerodynamic Performance and Loss Generation in a Three-Stage LP Turbine
GT 2001; V003T01A071https://doi.org/10.1115/2001-GT-0197
Topics:
Blades
,
Turbines
,
Separation (Technology)
,
Aircraft engines
,
Bubbles
,
Pressure
,
Reynolds number
,
Stress
,
Flow (Dynamics)
,
Guide vanes
Secondary Air Systems in Aeroengines Employing Vortex Reducers
GT 2001; V003T01A072https://doi.org/10.1115/2001-GT-0198
Topics:
Vortices
,
Compressors
,
Disks
,
Turbines
,
Pressure
,
Aircraft engines
,
Cavities
,
Computational fluid dynamics
,
Design
,
Engines
Approximate Solutions for Flow and Heat Transfer in Pre-Swirl Rotating-Disc Systems
GT 2001; V003T01A074https://doi.org/10.1115/2001-GT-0200
Topics:
Flow (Dynamics)
,
Heat transfer
,
Rotating disks
,
Disks
,
Cavities
,
Coolants
,
Cooling
,
Engines
,
Gas turbines
,
Momentum
Disintegration of Oil Films Emerging From Radial Holes in a Rotating Cylinder
GT 2001; V003T01A076https://doi.org/10.1115/2001-GT-0202
Topics:
Cylinders
,
Drops
,
Aircraft engines
,
Bearings
,
Boundary-value problems
,
Flow (Dynamics)
,
Rotating disks
,
Computational fluid dynamics
,
Databases
,
Design
Computational and Mathematical Modelling of Turbine Rim Seal Ingestion
GT 2001; V003T01A078https://doi.org/10.1115/2001-GT-0204
Topics:
Modeling
,
Turbines
,
Computational fluid dynamics
,
Annulus
,
Pressure
,
Accounting
,
Algorithms
,
Cavities
,
Disks
,
Flow (Dynamics)
Coupled Fluid/Solid Heat Transfer Computation for Turbine Discs
GT 2001; V003T01A079https://doi.org/10.1115/2001-GT-0205
Topics:
Computation
,
Disks
,
Fluids
,
Heat transfer
,
Turbines
,
Temperature
,
Engines
,
Heat transfer coefficients
,
Boundary-value problems
,
Cavities
Fundamental Design Issues of Brush Seals for Industrial Applications
Saim Dinc, Mehmet Demiroglu, Norman Turnquist, Jason Mortzheim, Gayle Goetze, John Maupin, James Hopkins, Christopher Wolfe, Mark Florin
GT 2001; V003T01A080https://doi.org/10.1115/2001-GT-0400
Topics:
Design
,
Failure mechanisms
,
Blades
,
Creep
,
Fatigue
,
High temperature
,
Oxidation
,
Stress
,
Tradeoffs
,
Turbines
Three Component Velocity Field Measurements in the Stagnation Region of a Film Cooled Turbine Vane
GT 2001; V003T01A082https://doi.org/10.1115/2001-GT-0402
Topics:
Turbines
,
Turbulence
,
Coolants
,
Jets
,
Flow (Dynamics)
,
Anisotropy
,
Fluctuations (Physics)
,
Gas turbines
,
Lasers
,
Test facilities
Conjugate Heat Transfer Analysis of Internally Cooled Configurations
GT 2001; V003T01A084https://doi.org/10.1115/2001-GT-0405
Topics:
Heat transfer
,
Flat plates
,
Flow (Dynamics)
,
Reynolds number
,
Coolants
,
Density
,
Heat flux
,
NASA
,
Pipe flow
,
Wall temperature
Turbulent Spots in Strong Adverse Pressure Gradients: Part 2 — Spot Propagation and Spreading Rates
GT 2001; V003T01A085https://doi.org/10.1115/2001-GT-0406
Topics:
Pressure gradient
,
Turbulence
,
Separation (Technology)
,
Turbomachinery
,
Blades
,
Boundary layers
,
Bubbles
,
Flat plates
,
Reynolds number
,
Wind tunnels
The Application of Printed Circuit Heat Exchanger Technology in the Pebble Bed Modular Reactor Demonstration Plant
GT 2001; V003T01A086https://doi.org/10.1115/2001-GT-0473
Topics:
Circuits
,
Heat exchangers
,
Cycles
,
Energy generation
,
Construction
,
Design
,
Diffusion (Physics)
,
Etching
,
Fluid dynamics
,
Helium
Pressure Field and Main-Stream Gas Ingestion in a Rotor-Stator Disk Cavity
GT 2001; V003T01A089https://doi.org/10.1115/2001-GT-0564
Topics:
Cavities
,
Disks
,
Pressure
,
Rotors
,
Stators
,
Engineering simulation
,
Simulation
,
Computational fluid dynamics
,
Blades
Gas Path Blade Tip Seals: Abradable Seal Material Testing at Utility Gas and Steam Turbine Operating Conditions
GT 2001; V003T01A090https://doi.org/10.1115/2001-GT-0583
Topics:
Blades
,
Sealants
,
Steam turbines
,
Testing
,
Gas turbines
,
Aerospace industry
,
Compressors
,
Erosion
,
Honeycomb structures
,
Leakage
On the Prediction of Secondary Flows in a U-Bend
GT 2001; V003T01A091https://doi.org/10.1115/2001-GT-0587
Topics:
Flow (Dynamics)
,
Turbulence
,
Interpolation
,
Reynolds number
,
Shear stress
Electric Power
Augmentation of Gas Turbine Power Output by Steam Injection
GT 2001; V003T02A001https://doi.org/10.1115/2001-GT-0107
Topics:
Gas turbines
,
Steam
,
Compressors
,
Flow (Dynamics)
,
Turbines
,
Combustion chambers
,
Cooling
,
Cycles
,
Exhaust systems
,
Heat
Qassim Central Power Plant Inlet Air Cooling System
GT 2001; V003T02A002https://doi.org/10.1115/2001-GT-0108
Topics:
Cooling systems
,
Power stations
,
Construction
,
Cooling
,
Flow (Dynamics)
,
Gas turbines
Applications of Gas Turbine Plants With Cooled Compressor Intake Air
GT 2001; V003T02A004https://doi.org/10.1115/2001-GT-0110
Topics:
Compressors
,
Gas turbines
,
Temperature
,
Cooling
,
Engines
,
Fuel consumption
Design Study of Part Flow Evaporative Gas Turbine Cycles: Performance and Equipment Sizing: Part 1 — Aeroderivative Core
GT 2001; V003T02A006https://doi.org/10.1115/2001-GT-0112
Topics:
Cycles
,
Design
,
Flow (Dynamics)
,
Gas turbines
,
Flue gases
,
Humidifiers
,
Air flow
,
Compressed air
,
Heat
,
Compressors
Design Study of Part Flow Evaporative Gas Turbine Cycles: Performance and Equipment Sizing: Part 2 — Industrial Core
GT 2001; V003T02A007https://doi.org/10.1115/2001-GT-0113
Topics:
Cycles
,
Design
,
Flow (Dynamics)
,
Gas turbines
,
Compressors
,
Humidifiers
,
Compressed air
,
Flue gases
,
Carbon dioxide
,
Cooling
Testing the Latest Model V84.3A Gas Turbine in the Siemens Test Facility in Berlin
GT 2001; V003T02A011https://doi.org/10.1115/2001-GT-0396
Topics:
Gas turbines
,
Test facilities
,
Testing
,
Stress
,
Aerodynamics
,
Blades
,
Combustion
,
Compressors
,
Engineering prototypes
,
Engines
CAES: Reduced to Practice
GT 2001; V003T02A012https://doi.org/10.1115/2001-GT-0397
Topics:
Air flow
,
Combustion
,
Combustion chambers
,
Compressed air
,
Dampers
,
Energy industry
,
Energy storage
,
Engineering prototypes
,
Exhaust systems
,
Flow (Dynamics)
Testing the World’s Largest Gas Turbines
GT 2001; V003T02A013https://doi.org/10.1115/2001-GT-0398
Topics:
Gas turbines
,
Testing
,
Building renovation
,
Construction
,
Engineering prototypes
,
Test facilities
Technical Risks and Mitigation Measures in Combustion Turbine Project Development
GT 2001; V003T02A016https://doi.org/10.1115/2001-GT-0472
Topics:
Combustion
,
Turbines
,
Risk
,
Maintenance
,
Fuels
,
Life cycle costing
,
Power stations
,
Profitability
,
Risk mitigation
Development of H Series Gas Turbine
GT 2001; V003T02A018https://doi.org/10.1115/2001-GT-0500
Topics:
Gas turbines
,
Cooling
,
Blades
,
Steam
,
Construction
,
Rotors
,
Stability
Demand Based Reliability: A Proposed Measurement Approach
GT 2001; V003T02A022https://doi.org/10.1115/2001-GT-0525
Topics:
Reliability
,
Profitability
,
Emissions
,
Energy generation
501F/M701F Gas Turbine Uprating
GT 2001; V003T02A024https://doi.org/10.1115/2001-GT-0553
Topics:
Gas turbines
,
Design
,
Combined cycles
,
Reliability
,
Combined cycle power stations
,
Countermeasures
,
Energy generation
,
Engines
,
Firing
,
Machinery
Evaluation and Comparison of Different Blade Cooling Solutions to Improve Cooling Efficiency and Gas Turbine Performances
GT 2001; V003T02A025https://doi.org/10.1115/2001-GT-0571
Topics:
Blades
,
Cooling
,
Gas turbines
,
Coolants
,
Design
,
Cooling systems
,
Engineering simulation
,
Reliability
,
Simulation
,
Steam
Industrial and Cogeneration
A Unique Approach for Thermo-Economic Optimization of an Intercooled, Reheat and Recuperated Gas Turbine for Cogeneration Applications
GT 2001; V003T03A001https://doi.org/10.1115/2001-GT-0206
Topics:
Combined heat and power
,
Gas turbines
,
Optimization
,
Thermoeconomics
,
Cycles
,
Heat
,
Stress
,
Sales
,
Brayton cycle
,
Design
Thermo-Economic Analysis of an Intercooled, Reheat and Recuperated Gas Turbine for Cogeneration Applications: Part II — Part-Load Operation
GT 2001; V003T03A002https://doi.org/10.1115/2001-GT-0207
Topics:
Combined heat and power
,
Gas turbines
,
Stress
,
Thermoeconomics
,
Cycles
,
Sales
,
Brayton cycle
,
Cogeneration systems
,
Design
,
Economic analysis
Multiobjective Robust Optimal Design of a Gas Turbine Cogeneration Plant Under Uncertain Energy Demands
GT 2001; V003T03A003https://doi.org/10.1115/2001-GT-0208
Topics:
Cogeneration plants
,
Design
,
Gas turbines
,
Design methodology
,
Energy consumption
,
Flow (Dynamics)
,
Linear programming
,
Optimization
,
Robustness
,
Tradeoffs
Thermo-Economic Optimization of a Cogeneration Plant With Below Ambient Pressure Discharge Gas Turbine
GT 2001; V003T03A004https://doi.org/10.1115/2001-GT-0209
Topics:
Cogeneration plants
,
Gas turbines
,
Optimization
,
Pressure
,
Thermoeconomics
,
Brayton cycle
,
Electricity (Physics)
,
Power stations
Heat Recovery System Control Strategy to Meet Multiple Transient Demands
GT 2001; V003T03A005https://doi.org/10.1115/2001-GT-0210
Topics:
Heat recovery
,
Transients (Dynamics)
,
Steam
,
Thermal efficiency
,
Turbines
,
Cooling
,
Gas turbines
,
Absorption
,
Capacitance
,
Dynamic models
Conformable Eddy-Current Sensors and Arrays for Fleetwide Gas Turbine Component Quality Assessment
Neil Goldfine, Darrell Schlicker, Yanko Sheiretov, Andrew Washabaugh, Vladimir Zilberstein, Timothy Lovett
GT 2001; V003T03A007https://doi.org/10.1115/2001-GT-0212
Topics:
Eddies (Fluid dynamics)
,
Eddy currents (Electricity)
,
Gas turbines
,
Sensors
,
Coating processes
,
Coatings
,
Blades
,
Failure
,
Inspection
,
Propellers
Heavy Fuel Operation at Limay Bataan Power Station
GT 2001; V003T03A008https://doi.org/10.1115/2001-GT-0213
Topics:
Fuels
,
Power stations
,
Combined cycles
,
Blades
,
Fuel oils
,
Teams
,
Turbines
,
Viscosity
Interstage Injection System for Heavy Duty Industrial Gas Turbine Model 7EA
GT 2001; V003T03A009https://doi.org/10.1115/2001-GT-0407
Topics:
Blades
,
Combined heat and power
,
Compressors
,
Detergents
,
Gas turbines
,
Industrial gases
,
Stress
,
Turbines
,
Water
Gas Turbine Inlet Air Cooling Using Absorption Refrigeration: A Comparison Based on a Combined Cycle Process
GT 2001; V003T03A010https://doi.org/10.1115/2001-GT-0408
Topics:
Absorption
,
Combined cycles
,
Cooling
,
Gas turbines
,
Refrigeration
,
Machinery
,
Evaporative cooling
,
Water
,
Compressors
,
Computer software
Options to Maximize Power Output for Merchant Plants in Combined Cycle Applications
GT 2001; V003T03A011https://doi.org/10.1115/2001-GT-0409
Topics:
Combined cycles
,
Power stations
,
Heat recovery steam generators
,
Cycles
,
Economics
,
Emissions
,
Energy generation
,
Energy industry
,
Firing
,
Fuels
Compressor Discharge Brush Seal for Gas Turbine Model 7EA
GT 2001; V003T03A012https://doi.org/10.1115/2001-GT-0410
Topics:
Compressors
,
Gas turbines
,
Compressed air
,
Diffusers
,
Industrial gases
,
Leakage
,
Pressure
,
Turbines
Experimental Investigation of an Inert Gas Generator for Fire Suppressing
GT 2001; V003T03A014https://doi.org/10.1115/2001-GT-0412
Topics:
Fire
,
Generators
,
Gas turbines
,
Temperature
,
Flow (Dynamics)
,
Oxygen
,
Water
,
Combustion
,
Cooling
,
Fuels
Improvement of the Accuracy in Gas Turbine Health Determination
GT 2001; V003T03A015https://doi.org/10.1115/2001-GT-0476
Topics:
Gas turbines
,
Monitoring systems
,
Sensors
,
Uncertainty
Economic and Technical Challenges Facing Large-Scale Gas Turbine Projects due to Environmental Requirements for Extremely Low Emissions
GT 2001; V003T03A017https://doi.org/10.1115/2001-GT-0591
Topics:
Emissions
,
Gas turbines
,
Combustion
,
Energy generation
,
Fossil fuels
,
Fuels
,
Gaseous fuels
,
Natural gas
,
Sulfur
,
Turbines