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Proceedings Papers
Volume 3: Heat Transfer; Electric Power; Industrial and Cogeneration
Heat Transfer
Leakage Flow Over Shrouded Turbine Blades
GT 2000; V003T01A001https://doi.org/10.1115/2000-GT-0193
Topics:
Leakage flows
,
Turbine blades
,
Flow (Dynamics)
,
Pressure
,
Navier-Stokes equations
,
Turbulence
Experimental Investigations on the Thermal Load and Leakage Flow of a Turbine Blade Tip Section With Different Tip Section Geometries
GT 2000; V003T01A004https://doi.org/10.1115/2000-GT-0196
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
GT 2000; V003T01A005https://doi.org/10.1115/2000-GT-0197
Topics:
Heat flux
,
Turbine blades
,
Blades
,
Pressure
,
Suction
,
Turbines
,
Chords (Trusses)
,
Design
,
Flow (Dynamics)
,
Heat transfer
Effects of Slot Bleed Injection Over a Contoured Endwall on Nozzle Guide Vane Cooling Performance: Part I — Flow Field Measurements
GT 2000; V003T01A007https://doi.org/10.1115/2000-GT-0199
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
GT 2000; V003T01A008https://doi.org/10.1115/2000-GT-0200
Topics:
Cooling
,
Nozzle guide vanes
,
Flow (Dynamics)
,
Airfoils
,
Combustion chambers
,
Coolants
,
Cascades (Fluid dynamics)
,
Chords (Trusses)
,
Convection
,
Design
An Investigation of Heat Transfer in a Film Cooled Transonic Turbine Cascade: Part I — Steady Heat Transfer
GT 2000; V003T01A010https://doi.org/10.1115/2000-GT-0202
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
GT 2000; V003T01A011https://doi.org/10.1115/2000-GT-0203
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
GT 2000; V003T01A012https://doi.org/10.1115/2000-GT-0204
Topics:
Gages
,
Heat flux
,
Heat transfer
,
Liquid crystals
,
Nozzle guide vanes
,
Surface roughness
,
Heat transfer coefficients
,
Cooling
,
Engines
,
Film cooling
Influence of Vane/Blade Spacing on the Heat Flux for a Transonic Turbine
GT 2000; V003T01A014https://doi.org/10.1115/2000-GT-0206
Topics:
Blades
,
Heat flux
,
Turbines
,
Pressure
,
Chords (Trusses)
,
Heat
,
Reynolds number
,
Stress
Cooling Effectiveness Measurements With Thermal Radiometry in a Turbine Cascade
GT 2000; V003T01A015https://doi.org/10.1115/2000-GT-0207
Topics:
Cascades (Fluid dynamics)
,
Cooling
,
Radiation measurement
,
Turbines
,
Airfoils
,
Temperature
,
Coolants
,
Engines
,
Thermocouples
,
Background radiation
Heat Transfer Measurements and Predictions on a Power Generation Gas Turbine Blade
GT 2000; V003T01A017https://doi.org/10.1115/2000-GT-0209
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
GT 2000; V003T01A018https://doi.org/10.1115/2000-GT-0210
Topics:
Aerodynamics
,
Design
,
Heat transfer
,
Turbine blades
,
Flow (Dynamics)
,
Navier-Stokes equations
,
Numerical analysis
,
Algorithms
,
Blades
,
Momentum
Augmentation of Stagnation Region Heat Transfer due to Turbulence From a DLN Can Combustor
GT 2000; V003T01A023https://doi.org/10.1115/2000-GT-0215
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
GT 2000; V003T01A024https://doi.org/10.1115/2000-GT-0216
Topics:
Heat transfer
,
Low temperature
,
Surface roughness
,
Turbines
,
Cascades (Fluid dynamics)
,
Heat conduction
,
Mach number
,
Pressure
,
Suction
,
Temperature
Experimental Investigation on Impingement Heat Transfer From Rib Roughened Surface Within Arrays of Circular Jets: Correlation
GT 2000; V003T01A028https://doi.org/10.1115/2000-GT-0220
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
GT 2000; V003T01A029https://doi.org/10.1115/2000-GT-0221
Topics:
Heat transfer
,
Steam
,
Cooling
,
Reynolds number
,
Blades
,
Drops
,
Flux (Metallurgy)
,
Heat
,
Turbines
,
Wall temperature
Flow and Heat Transfer of Confined Impingement Jets Cooling
GT 2000; V003T01A031https://doi.org/10.1115/2000-GT-0223
Topics:
Cooling
,
Flow (Dynamics)
,
Heat transfer
,
Jets
,
Heat transfer coefficients
,
Reynolds number
,
Cavities
,
Convection
,
Cross-flow
,
Liquid crystals
Application of Non-Linear k–ω Model to the Turbulent Flow Inside a Sharp U-Bend
GT 2000; V003T01A033https://doi.org/10.1115/2000-GT-0225
Topics:
Turbulence
,
Flow (Dynamics)
,
Anisotropy
,
Ducts
,
Interpolation
,
Shear stress
,
Simulation
Rotating Effect on Fluid Flow in a Smooth Duct With a 180-Deg Sharp Turn
GT 2000; V003T01A036https://doi.org/10.1115/2000-GT-0228
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
GT 2000; V003T01A037https://doi.org/10.1115/2000-GT-0229
Topics:
Flow (Dynamics)
,
Heat transfer
,
Stress
,
Turbulence
,
Buoyancy
,
Computation
,
Coolants
,
Coriolis force
,
Corners (Structural elements)
,
Density
Lateral-Flow Effect on Endwall Heat Transfer and Pressure Drop in a Pin-Fin Trapezoidal Duct of Various Pin Shapes
GT 2000; V003T01A040https://doi.org/10.1115/2000-GT-0232
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
GT 2000; V003T01A041https://doi.org/10.1115/2000-GT-0233
Topics:
Cooling
,
Heat transfer
,
Temperature measurement
,
Temperature
,
Strips
,
Turbine blades
,
External pressure
,
Film cooling
,
Liquid crystals
,
Steady state
Influence of Cross-Flow Induced Swirl and Impingement on Heat Transfer in a Two-Pass Channel Connected by Two Rows of Holes
GT 2000; V003T01A043https://doi.org/10.1115/2000-GT-0235
Topics:
Cross-flow
,
Heat transfer
,
Coolants
,
Channel flow
,
Cooling
,
Design
,
Flow (Dynamics)
,
Heat transfer coefficients
,
Liquid crystals
,
Reynolds number
Innovative Cyclone Cooling Scheme for Gas Turbine Blade: Thermal-Hydraulic Performance Evaluation
GT 2000; V003T01A045https://doi.org/10.1115/2000-GT-0237
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
GT 2000; V003T01A046https://doi.org/10.1115/2000-GT-0238
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
GT 2000; V003T01A047https://doi.org/10.1115/2000-GT-0239
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
GT 2000; V003T01A048https://doi.org/10.1115/2000-GT-0240
Topics:
Film cooling
,
Coolants
,
Pressure
,
Turbulence
,
Airfoils
,
Turbines
,
Boundary layers
,
Cooling
,
Density
,
Flat plates
Novel Blade Cooling Engineering Solution
GT 2000; V003T01A049https://doi.org/10.1115/2000-GT-0242
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
GT 2000; V003T01A050https://doi.org/10.1115/2000-GT-0243
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
GT 2000; V003T01A051https://doi.org/10.1115/2000-GT-0244
Topics:
Coatings
,
Film cooling
,
Turbines
,
Airfoils
,
Coolants
,
Cross section (Physics)
,
Databases
,
Diffusers
,
Flat plates
,
Flow (Dynamics)
The Effects of Injection Angle and Hole Exit Shape on Turbine Nozzle Pressure Side Film Cooling
GT 2000; V003T01A053https://doi.org/10.1115/2000-GT-0247
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
GT 2000; V003T01A054https://doi.org/10.1115/2000-GT-0248
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
GT 2000; V003T01A055https://doi.org/10.1115/2000-GT-0249
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
GT 2000; V003T01A056https://doi.org/10.1115/2000-GT-0250
Topics:
Temperature
,
Turbines
,
Cooling
,
Flow (Dynamics)
,
Blades
,
Combustion chambers
,
Gas turbines
Thermal Conjugate Analysis of a First Stage Blade in a Gas Turbine
GT 2000; V003T01A057https://doi.org/10.1115/2000-GT-0251
Topics:
Blades
,
Gas turbines
,
Temperature
,
Cooling
,
Numerical analysis
,
Air flow
,
Convection
,
Heat
,
Heat conduction
,
Heat transfer
Simultaneous Prediction of External Flow-Field and Temperature in Internally Cooled 3-D Turbine Blade Material
GT 2000; V003T01A059https://doi.org/10.1115/2000-GT-0253
Topics:
Flow (Dynamics)
,
Temperature
,
Turbine blades
,
Convection
,
Coolants
,
Heat transfer
,
Airfoils
,
Blades
,
Boundary-value problems
,
Computers
Heat Transfer Analysis in a Modern DLN Combustor
GT 2000; V003T01A060https://doi.org/10.1115/2000-GT-0254
Topics:
Combustion chambers
,
Heat transfer
,
Cooling
,
Emissions
,
Air flow
,
Flow (Dynamics)
,
Fuels
,
Pressure
,
Compressors
,
Convection
Turbulence Structures of Leading Edge Film Cooling Jets
GT 2000; V003T01A061https://doi.org/10.1115/2000-GT-0255
Topics:
Film cooling
,
Jets
,
Turbulence
,
Pressure
,
Blades
,
Suction
,
Anisotropy
,
Cascades (Fluid dynamics)
,
Coolants
,
Diffusion (Physics)
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
GT 2000; V003T01A064https://doi.org/10.1115/2000-GT-0258
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
GT 2000; V003T01A065https://doi.org/10.1115/2000-GT-0260
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
GT 2000; V003T01A066https://doi.org/10.1115/2000-GT-0261
Topics:
Pressure
,
Turbines
,
Wakes
,
Boundary layers
,
Blades
,
Cascades (Fluid dynamics)
,
Inflow
,
Engines
,
Reynolds number
,
Simulation
Turbine Separation Control Using Pulsed Vortex Generator Jets
GT 2000; V003T01A067https://doi.org/10.1115/2000-GT-0262
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
GT 2000; V003T01A068https://doi.org/10.1115/2000-GT-0263
Topics:
Boundary layers
,
Cascades (Fluid dynamics)
,
Compressors
,
Reynolds number
,
Turbulence
,
Blades
,
Chords (Trusses)
,
Airfoils
,
Bubbles
,
Coatings
Natural Transition Phenomena on an Axial Compressor Blade
GT 2000; V003T01A069https://doi.org/10.1115/2000-GT-0264
Topics:
Blades
,
Compressors
,
Waves
,
Algorithms
,
Turbulence
,
Flow (Dynamics)
,
Inflow
,
Inlet guide vanes
,
Probability
,
Stators
Control of Separation Bubble on a Blade Leading Edge by a Stationary Bar Wake
GT 2000; V003T01A072https://doi.org/10.1115/2000-GT-0267
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
GT 2000; V003T01A073https://doi.org/10.1115/2000-GT-0268
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
GT 2000; V003T01A074https://doi.org/10.1115/2000-GT-0269
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
GT 2000; V003T01A075https://doi.org/10.1115/2000-GT-0270
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
GT 2000; V003T01A076https://doi.org/10.1115/2000-GT-0271
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
GT 2000; V003T01A077https://doi.org/10.1115/2000-GT-0272
Topics:
Boundary layers
,
Turbulence
,
Wakes
,
Probes
,
Wire
,
Flat plates
,
Fluctuations (Physics)
,
Sensors
,
Shear stress
A Study on Models to Simulate Boundary Layer Transition in Turbomachinery Flows
GT 2000; V003T01A079https://doi.org/10.1115/2000-GT-0274
Topics:
Boundary layers
,
Flow (Dynamics)
,
Turbomachinery
,
Modeling
,
Turbulence
,
Cascades (Fluid dynamics)
,
Compressors
,
Computation
,
Stability
,
Steady state
Droplet Generation by Disintegration of Oil Films at the Rim of a Rotating Disk
GT 2000; V003T01A083https://doi.org/10.1115/2000-GT-0279
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
GT 2000; V003T01A084https://doi.org/10.1115/2000-GT-0280
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
GT 2000; V003T01A085https://doi.org/10.1115/2000-GT-0281
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
GT 2000; V003T01A086https://doi.org/10.1115/2000-GT-0282
Topics:
Cavities
,
Engines
,
Heat transfer
,
Heat conduction
,
Rotors
,
Aircraft engines
,
Blades
,
Computation
,
Cooling
,
Cooling systems
Total Pressure Losses in Rotor Systems With Radial Inflow
GT 2000; V003T01A087https://doi.org/10.1115/2000-GT-0283
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
GT 2000; V003T01A088https://doi.org/10.1115/2000-GT-0284
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
GT 2000; V003T01A089https://doi.org/10.1115/2000-GT-0285
Topics:
Cavities
,
Flow (Dynamics)
,
Heat transfer
,
Rotors
,
Sealing (Process)
,
Stators
,
Computational fluid dynamics
,
Disks
,
Engines
,
Steady state
Influence of a Honeycomb Facing on the Heat Transfer in a Stepped Labyrinth Seal
GT 2000; V003T01A091https://doi.org/10.1115/2000-GT-0290
Topics:
Heat transfer
,
Honeycomb structures
,
Heat transfer coefficients
,
Stators
,
Flow (Dynamics)
,
Geometry
,
Engines
,
Finite element analysis
,
Jet engines
,
Pressure
Large-Scale Testing to Validate the Influence of External Crossflow on the Discharge Coefficients of Film Cooling Holes
GT 2000; V003T01A094https://doi.org/10.1115/2000-GT-0293
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
GT 2000; V003T01A095https://doi.org/10.1115/2000-GT-0294
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
GT 2000; V003T01A096https://doi.org/10.1115/2000-GT-0295
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
GT 2000; V003T01A097https://doi.org/10.1115/2000-GT-0296
Topics:
Cascades (Fluid dynamics)
,
Suction
,
Turbines
,
Heat transfer
,
Flow (Dynamics)
,
Steady state
,
Aerodynamics
,
Boundary layers
,
Film cooling
,
Gas turbines
Control of Secondary Flows in a Turbine Nozzle Guide Vane by Endwall Contouring
GT 2000; V003T01A101https://doi.org/10.1115/2000-GT-0556
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
GT 2000; V003T01A102https://doi.org/10.1115/2000-GT-0557
Topics:
Aerodynamics
,
Coolants
,
Pressure
,
Turbine blades
,
Wakes
,
Blades
,
Flow (Dynamics)
,
Turbulence
,
Algebra
,
Computer simulation
Detailed Flow and Heat Transfer Coefficient Measurements in a Model of an Internal Cooling Geometry Employing Orthogonal Intersecting Channels
GT 2000; V003T01A104https://doi.org/10.1115/2000-GT-0653
Topics:
Cooling
,
Flow (Dynamics)
,
Geometry
,
Heat transfer coefficients
,
Engines
,
Reynolds number
,
Temperature
,
Airfoils
,
Film cooling
,
Gas turbines
Electric Power
Managing Fuel Oil Nozzle Coking to Improve Gas Turbine Availability
GT 2000; V003T02A002https://doi.org/10.1115/2000-GT-0177
Topics:
Fuel management
,
Gas turbines
,
Nozzles
,
Fuel oils
,
Cooling
,
Power stations
,
Engines
,
Fuels
,
Inspection
,
Motors
Early Detection of Combustor Pulsations and Optimized Operation Through On-Line Monitoring Systems
GT 2000; V003T02A004https://doi.org/10.1115/2000-GT-0180
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
GT 2000; V003T02A005https://doi.org/10.1115/2000-GT-0181
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
GT 2000; V003T02A006https://doi.org/10.1115/2000-GT-0182
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
GT 2000; V003T02A007https://doi.org/10.1115/2000-GT-0184
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
GT 2000; V003T02A008https://doi.org/10.1115/2000-GT-0185
Topics:
Artificial neural networks
,
Gas turbines
,
Heat recovery
,
Algorithms
,
Boilers
,
Feedforward control
,
Instrumentation
,
Optimization
,
Power stations
,
Steady state
Risk-Based Inspection of Combustion Turbines
GT 2000; V003T02A011https://doi.org/10.1115/2000-GT-0189
Topics:
Combustion
,
Risk-based inspection
,
Turbines
,
Reliability
,
Maintenance
,
Risk
,
Algorithms
,
Inspection
,
Machinery
,
Mechanical engineers
Experience With a Fast Track Power Generation Project
GT 2000; V003T02A017https://doi.org/10.1115/2000-GT-0591
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
Topics:
Gas turbines
,
Heat recovery steam generators
,
Pressure
,
Design
,
Reliability
,
Stress
,
Combined cycle gas turbines
,
Optimization
,
Simulation
,
Temperature
The Single-Shaft Combined Cycle Myth
GT 2000; V003T02A020https://doi.org/10.1115/2000-GT-0594
Alabama Electric Cooperative Compressed Air Energy Storage (CAES) Plant Improvements
GT 2000; V003T02A021https://doi.org/10.1115/2000-GT-0595
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
GT 2000; V003T02A022https://doi.org/10.1115/2000-GT-0596
Topics:
Combustion
,
Combustion chambers
,
Energy storage
,
Gas turbines
,
Heat
,
Power stations
,
Temperature
,
Turbines
Use of Unconventional Fuels in Gas Turbines
GT 2000; V003T02A023https://doi.org/10.1115/2000-GT-0637
Topics:
Fuels
,
Gas turbines
,
Combustion
,
Condensed matter
,
Design
,
Blast furnaces
,
China
,
Combined cycle power stations
,
Combined cycles
,
Combustion chambers
Industrial and Cogeneration
Spinning Reserve Influence in a Power Generating System Integrated by Hydro Storage Plants
GT 2000; V003T03A002https://doi.org/10.1115/2000-GT-0300
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
GT 2000; V003T03A003https://doi.org/10.1115/2000-GT-0301
Topics:
Cogeneration plants
,
Combined cycles
,
Cycles
,
Steam
,
Economics
,
Energy generation
,
Flow (Dynamics)
,
Combined heat and power
,
Energy industry
,
Gas turbines
Application of Evaporative Coolers for Gas Turbine Power Plants
GT 2000; V003T03A005https://doi.org/10.1115/2000-GT-0303
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
GT 2000; V003T03A006https://doi.org/10.1115/2000-GT-0304
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
GT 2000; V003T03A007https://doi.org/10.1115/2000-GT-0305
Topics:
Gas turbines
,
Water
,
Compressors
,
Particulate matter
,
Compression
,
Evaporation
,
Information Analysis Centers
,
Inlet guide vanes
,
Machinery
,
Pressure
Gas Turbine Field Performance Determination: Sources of Uncertainties
GT 2000; V003T03A012https://doi.org/10.1115/2000-GT-0311
Topics:
Gas turbines
,
Uncertainty
,
Errors
,
Thermodynamic cycles
Real-Time On-Line Performance Diagnostics of Heavy-Duty Industrial Gas Turbines
GT 2000; V003T03A013https://doi.org/10.1115/2000-GT-0312
Topics:
Cogeneration plants
,
Combined cycles
,
Compressors
,
Computer software
,
Control systems
,
Databases
,
Engines
,
Filters
,
Gas turbines
,
Industrial gases
Remote Monitoring and Diagnostics System for GE Heavy Duty Gas Turbines
GT 2000; V003T03A015https://doi.org/10.1115/2000-GT-0314
Topics:
Gas turbines
,
Design
,
Algorithms
,
Combustion
,
Computers
,
Energy generation
,
Maintenance
,
Power stations
,
Turbines
,
Vibration
Thermo-Economic Analysis of an Intercooled, Reheat and Recuperated Gas Turbine for Cogeneration Applications: Part I — Base Load Operation
GT 2000; V003T03A017https://doi.org/10.1115/2000-GT-0316
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)
GT 2000; V003T03A018https://doi.org/10.1115/2000-GT-0317
Topics:
Exergy
,
Gas turbines
,
Liquefied natural gas
,
Mirrors
,
Cycles
,
Seawater
,
Brayton cycle
,
Climate change
,
Combined cycles
,
Evaporation
A Steady State Calculation Model for Gas Turbine Thermal Enclosures
GT 2000; V003T03A021https://doi.org/10.1115/2000-GT-0320
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
GT 2000; V003T03A022https://doi.org/10.1115/2000-GT-0558
Topics:
Bearings
,
Gas turbines
,
Rotors
,
Leakage
,
Cavities
,
Compressors
,
Polishing equipment
,
High pressure (Physics)
,
Journal bearings
,
Lubricating oils