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Proceedings Papers
In This Volume
Volume 5A: Heat Transfer
Conjugate Heat Transfer
Large-Eddy Simulation and Conjugate Heat Transfer in a Round Impinging Jet
GT 2014; V05AT11A001https://doi.org/10.1115/GT2014-25152
Topics:
Heat transfer
,
Large eddy simulation
,
Engineering simulation
,
Heat flux
,
Simulation
,
Unsteady flow
,
Boundary layers
,
Computation
,
Finishes
,
Flow (Dynamics)
Conjugate Heat Transfer Characteristics of a Highly Thermal-Loaded Film Cooling System in Hot and Multi-Composition Gas Condition
GT 2014; V05AT11A002https://doi.org/10.1115/GT2014-25187
Topics:
Film cooling
,
Heat transfer
,
Radiation (Physics)
,
Temperature
,
Convection
,
Emissions
,
Heat
,
Heat conduction
,
Steam
,
Flow (Dynamics)
Conjugate Heat Transfer Predictions of Effusion Cooling With Shaped Trench Outlet
GT 2014; V05AT11A003https://doi.org/10.1115/GT2014-25257
Topics:
Cooling
,
Heat transfer
,
Design
,
Computational fluid dynamics
,
Film cooling
,
Adiabatic cooling
,
Coolants
,
Flow (Dynamics)
,
Gas turbines
,
Metal surfaces
Conjugate Heat Transfer CFD Predictions of Impingement Heat Transfer: Influence of the Number of Holes for a Constant Pitch-to-Diameter Ratio X/D
GT 2014; V05AT11A004https://doi.org/10.1115/GT2014-25268
Topics:
Computational fluid dynamics
,
Heat transfer
,
Combustion chambers
,
Coolants
,
Cross-flow
,
Flow (Dynamics)
,
Temperature gradient
,
Air flow
,
Capacitance
,
Density
Conjugate Heat Transfer CFD Predictions of Impingement Heat Transfer: The Influence of Hole Pitch to Diameter Ratio X/D at Constant Impingement Gap Z
GT 2014; V05AT11A005https://doi.org/10.1115/GT2014-25269
Topics:
Computational fluid dynamics
,
Heat transfer
,
Flow (Dynamics)
,
Heat transfer coefficients
,
Coolants
,
Cooling
,
Metals
,
Pressure
,
Aerodynamics
,
Capacitance
Aerothermal Analysis of a Turbine With Rim Seal Cavity
GT 2014; V05AT11A006https://doi.org/10.1115/GT2014-25276
Topics:
Cavities
,
Turbines
,
Flow (Dynamics)
,
Computation
,
Sealing (Process)
,
Blades
,
Annulus
,
Boundary-value problems
,
Computational fluid dynamics
,
Disks
The Effect of Aircraft Integration Design on Gas Turbine Shaft Thermal Bow and the Newkirk Effect
GT 2014; V05AT11A009https://doi.org/10.1115/GT2014-25511
Topics:
Aircraft
,
Design
,
Gas turbines
,
Computational fluid dynamics
,
Finite element analysis
,
Cooling
,
Deformation
,
Temperature
,
Thermal expansion
,
Blades
Reverse-Pass Cooling Systems for Improved Performance
GT 2014; V05AT11A011https://doi.org/10.1115/GT2014-25901
Topics:
Blades
,
Combustion chambers
,
Coolants
,
Cooling
,
Cooling systems
,
Engine design
,
Engines
,
Film cooling
,
Flat plates
,
Flow (Dynamics)
Conjugate Heat Transfer Analysis for Gas Turbine Cooled Blade
GT 2014; V05AT11A012https://doi.org/10.1115/GT2014-25952
Topics:
Blades
,
Gas turbines
,
Heat transfer
,
Temperature
,
Metals
,
Airfoils
,
Computational fluid dynamics
,
Cooling
,
Engines
,
Flow (Dynamics)
Numerical Analysis of Oil Anti-Icing System Performance of Turboshaft Engine Inlet Strut
GT 2014; V05AT11A015https://doi.org/10.1115/GT2014-26564
Topics:
Engines
,
Numerical analysis
,
Struts (Engineering)
,
Computation
,
Temperature
,
Flow (Dynamics)
,
Heat transfer
,
Water
,
Air flow
,
Computational fluid dynamics
Conjugate Heat Transfer Analysis in an Actual Gas Turbine Rotor Blade in Comparison With Pyrometer Data
GT 2014; V05AT11A016https://doi.org/10.1115/GT2014-26962
Topics:
Blades
,
Gas turbines
,
Heat transfer
,
Pyrometers
,
Rotors
,
Flow (Dynamics)
,
Temperature distribution
,
Cooling
,
Fluids
,
Pressure
Internal Cooling
Investigations on Fluid Flow and Heat Transfer Performances Within a Real Turbine Blade Channel
GT 2014; V05AT12A001https://doi.org/10.1115/GT2014-25097
Topics:
Fluid dynamics
,
Heat transfer
,
Turbine blades
,
Flow (Dynamics)
,
Reynolds number
,
Rotation
,
Pressure
,
Blades
,
Computer software
,
Cross section (Physics)
PIV Measurements in a Two-Pass 90-Deg Ribbed-Wall Parallelogram Channel
GT 2014; V05AT12A003https://doi.org/10.1115/GT2014-25248
Topics:
Blades
,
Bubbles
,
Cooling
,
Flow (Dynamics)
,
Gas turbines
,
Heat transfer
,
Kinetic energy
,
Particulate matter
,
Reynolds number
,
Rotors
Thermal Performance of a Radially Rotating Twin-Pass Smooth-Walled Parallelogram Channel
GT 2014; V05AT12A004https://doi.org/10.1115/GT2014-25322
Topics:
Blades
,
Buoyancy
,
Cooling
,
Flow (Dynamics)
,
Friction
,
Heat transfer
,
Rotors
,
Turbines
The Effect of Vortex Core Distribution on Heat Transfer in Steam Cooling of Gas Turbine Blade Internal Ribbed Channels
GT 2014; V05AT12A005https://doi.org/10.1115/GT2014-25324
Topics:
Blades
,
Cooling
,
Gas turbines
,
Heat transfer
,
Steam
,
Vortices
,
Flow (Dynamics)
,
Shapes
,
Heat
,
Mass transfer
Row Removal Heat Transfer Study for Pin Fin Arrays
GT 2014; V05AT12A006https://doi.org/10.1115/GT2014-25348
Topics:
Heat transfer
,
Fins
,
Pins (Engineering)
,
Channel flow
,
Circular cylinders
,
Flow (Dynamics)
,
Heat
,
Reynolds number
,
Shapes
,
Turbines
Experimental Study on Local Heat Transfer in a Rotating, Two-Pass Cooling Channel With Dense Array of Turbulence Promoters With Naphthalene Sublimation Method
GT 2014; V05AT12A008https://doi.org/10.1115/GT2014-25369
Topics:
Cooling
,
Heat transfer
,
Turbulence
,
Heat transfer coefficients
,
Rotation
,
Mass transfer
,
Airfoils
,
Displacement
,
Heat
,
Lasers
Heat Transfer Measurements of Oblong Pins
GT 2014; V05AT12A009https://doi.org/10.1115/GT2014-25370
Topics:
Heat transfer
,
Pins (Engineering)
,
Blades
,
Fins
,
Flow (Dynamics)
,
Gas turbines
,
Shapes
Heat Transfer and Pressure Loss Measurements of Matrix Cooling Geometries for Gas Turbine Airfoils
GT 2014; V05AT12A010https://doi.org/10.1115/GT2014-25384
Topics:
Airfoils
,
Cooling
,
Gas turbines
,
Heat transfer
,
Pressure
,
Pressure drop
,
Reynolds number
,
Chords (Trusses)
,
Cooling systems
,
Flow (Dynamics)
Numerical Study of Turbulent Flow Through Rib-Roughened Channels With Mist Injection
GT 2014; V05AT12A011https://doi.org/10.1115/GT2014-25408
Topics:
Turbulence
,
Steam
,
Heat transfer
,
Computation
,
Cooling
,
Cross section (Physics)
,
Finite volume methods
,
Fluids
,
Heat flux
,
Heat transfer coefficients
Comparative Study of Impinging Jet Array Heat Transfer on a Flat Plate Cooled by Superheated Steam and Air
GT 2014; V05AT12A013https://doi.org/10.1115/GT2014-25493
Topics:
Flat plates
,
Heat transfer
,
Steam
,
Superheating
,
Cooling
,
Flow (Dynamics)
,
Computer simulation
,
Heat transfer coefficients
,
Combustion chambers
,
Compressors
Effect of Corrugated Orifice and Pin-Fin on Multiple Array Impingement Cooling With Low Nozzle to Target Distance
GT 2014; V05AT12A014https://doi.org/10.1115/GT2014-25494
Topics:
Impingement cooling
,
Nozzles
,
Fins
,
Heat transfer
,
Pressure drop
,
Simulation
,
Temperature
,
Turbines
,
Combustion chambers
,
Cooling
Heat Transfer in a Vane Trailing Edge Passage With Conical Pins and Pin-Turbulator Integrated Configurations
GT 2014; V05AT12A015https://doi.org/10.1115/GT2014-25522
Topics:
Heat transfer
,
Pins (Engineering)
,
Heat transfer coefficients
,
Pressure drop
,
Flow (Dynamics)
,
Gas turbines
,
Pressure
,
Temperature
,
Blades
,
Coolants
Investigation of Applicability of Transporting Water Mist for Cooling Turbine Blades
GT 2014; V05AT12A021https://doi.org/10.1115/GT2014-25818
Topics:
Cooling
,
Turbine blades
,
Water
,
Blades
,
Computational fluid dynamics
,
Gas turbines
,
Cavities
,
Diaphragms (Mechanical devices)
,
Diaphragms (Structural)
,
Drops
Effect of Rotation on Heat Transfer and Flow Field Inside Leading Edge Cooling Passage Using Impinging Jets
GT 2014; V05AT12A022https://doi.org/10.1115/GT2014-25824
Topics:
Cooling
,
Flow (Dynamics)
,
Heat transfer
,
Jets
,
Rotation
,
Blades
,
Computational fluid dynamics
,
Engineering simulation
,
Mach number
,
Simulation
Impact of Turbulator Design on the Heat Transfer in a High Aspect Ratio Passage of a Turbine Blade
GT 2014; V05AT12A023https://doi.org/10.1115/GT2014-25841
Topics:
Design
,
Heat transfer
,
Turbine blades
,
Heat transfer coefficients
,
Pressure
,
Pressure drop
,
Temperature
,
Blades
,
Coolants
,
Cooling
Leading Edge Cooling of a Gas Turbine Blade With Double Swirl Chambers
GT 2014; V05AT12A024https://doi.org/10.1115/GT2014-25851
Topics:
Blades
,
Cooling
,
Gas turbines
,
Flow (Dynamics)
,
Heat transfer
,
Impingement cooling
,
Coolants
,
Heat flux
,
Pressure
,
Reynolds number
Heat Transfer Enhancement Using Wedge-Shaped Detached Ribs With Grooves in Internal Cooling Channel
GT 2014; V05AT12A025https://doi.org/10.1115/GT2014-25863
Topics:
Cooling
,
Heat transfer
,
Wedges
,
Corners (Structural elements)
,
Flow (Dynamics)
,
Blades
,
Boundary-value problems
,
Dimensions
,
Gas turbines
,
Heat
Detailed Heat Transfer Distributions of Narrow Impingement Channels With Varying Jet Diameter
GT 2014; V05AT12A028https://doi.org/10.1115/GT2014-25910
Topics:
Heat transfer
,
Airfoils
,
Coolants
,
Cooling
,
Design
,
Discharge coefficient
,
Geometry
,
Heat transfer coefficients
,
Jets
,
Liquid crystals
Numerical and Experimental Investigation for Internal Cooling of Two Pass Gas Turbine Blades Channels Using Broken V Ribs
GT 2014; V05AT12A030https://doi.org/10.1115/GT2014-26147
Topics:
Blades
,
Cooling
,
Gas turbines
,
Temperature
,
Ducts
,
Heat transfer
,
High temperature
,
Reynolds number
,
Thermal efficiency
,
Thermal stresses
Experimental Investigation of a Leading Edge Cooling System With Optimized Inclined Racetrack Holes
GT 2014; V05AT12A034https://doi.org/10.1115/GT2014-26219
Topics:
Cooling systems
,
Cavities
,
Cooling
,
Engines
,
Film cooling
,
Flow (Dynamics)
,
Geometry
,
Heat transfer
,
High pressure (Physics)
,
Liquid crystals
Unsteady RANS Analysis of Particles Deposition in the Coolant Channel of a Gas Turbine Blade Using a Non-Linear Model
GT 2014; V05AT12A035https://doi.org/10.1115/GT2014-26252
Topics:
Blades
,
Coolants
,
Gas turbines
,
Particulate matter
,
Reynolds-averaged Navier–Stokes equations
,
Flow (Dynamics)
,
Cooling
,
Algorithms
,
Ash
,
Compressors
Wireless Telemetric Data Acquisition and Real-Time Control for a High Measurement-Density Internal Heat Transfer Experiment
GT 2014; V05AT12A036https://doi.org/10.1115/GT2014-26408
Topics:
Data acquisition
,
Density
,
Heat transfer
,
Real-time control
,
Signals
,
Control systems
,
Feedback
,
Temperature
,
Batteries
,
Construction
Crossflows From Jet Array Impingement Cooling: Effects of Hole Array Spacing, Jet-to-Target Plate Distance, and Reynolds Number
GT 2014; V05AT12A037https://doi.org/10.1115/GT2014-26426
Topics:
Impingement cooling
,
Reynolds number
,
Jets
,
Cross-flow
,
Shear (Mechanics)
,
Heat transfer
,
Turbulence
,
Vortices
Numerical Studies on Effect of Channel Orientation in a Rotating Smooth Wedge-Shaped Cooling Channel
GT 2014; V05AT12A039https://doi.org/10.1115/GT2014-26560
Topics:
Cooling
,
Wedges
,
Heat transfer
,
Turbine blades
,
Rotation
,
Computational fluid dynamics
,
Fins
,
Gas turbines
,
Heat transfer coefficients
,
Temperature
Effect of Entrance Geometry and Rotation on Heat Transfer in a Narrow (AR = 1:4) Rectangular Internal Cooling Channel
GT 2014; V05AT12A040https://doi.org/10.1115/GT2014-26602
Topics:
Cooling
,
Geometry
,
Heat transfer
,
Rotation
,
Flow (Dynamics)
,
Computer simulation
,
Shapes
,
Blades
,
Density
,
Fluid dynamics
Numerical Study of Impingement and Film Composite Cooling on Blade Leading Edge
GT 2014; V05AT12A042https://doi.org/10.1115/GT2014-26643
Topics:
Blades
,
Composite materials
,
Cooling
,
Density
,
Shear stress
,
Simulation
,
Computational fluid dynamics
,
Computer software
,
Engines
,
High pressure (Physics)
Friction and Heat Transfer in a Rotating Rib-Roughened Square U-Duct Under High Rotation Numbers
GT 2014; V05AT12A043https://doi.org/10.1115/GT2014-26663
Topics:
Ducts
,
Friction
,
Heat transfer
,
Rotation
,
Copper
,
Heat transfer coefficients
,
Pressure
,
Pressure drop
,
Pressure measurement
,
Reynolds number
Heat Transfer and Pressure Loss Characteristics of a Narrow Internal Cooling Passage at Low Reynolds Number
GT 2014; V05AT12A047https://doi.org/10.1115/GT2014-27077
Topics:
Cooling
,
Heat transfer
,
Pressure
,
Reynolds number
,
Airfoils
,
Computational fluid dynamics
,
Computer software
,
Dimensions
,
Flow (Dynamics)
,
Gas turbines
Heat Transfer and Friction Studies in a Tilted and Rib-Roughened Trailing-Edge Cooling Cavity With and Without the Trailing-Edge Cooling Holes
GT 2014; V05AT12A048https://doi.org/10.1115/GT2014-27130
Topics:
Cavities
,
Cooling
,
Friction
,
Heat transfer
,
Airfoils
,
Boundary-value problems
,
Flow (Dynamics)
,
Heat transfer coefficients
,
Pressure
,
Turbulence
Particle Deposition in Internal Cooling Cavities of a Nozzle Guide Vane: Part I — Experimental Investigation
GT 2014; V05AT12A049https://doi.org/10.1115/GT2014-27150
Topics:
Cavities
,
Cooling
,
Nozzle guide vanes
,
Particulate matter
,
Flow (Dynamics)
,
Jets
,
Temperature
,
Heating
,
Impingement cooling
,
Low temperature
Heat Transfer in Rotating Two-Pass Channel With Bleed Holes on Tip Surface
Ho-Seong Sohn, Namgeon Yun, Jun Su Park, Hyung Hee Cho, Kyung Min Kim, Beom Soo Kim, Byung Moon Jang
GT 2014; V05AT12A051https://doi.org/10.1115/GT2014-27254
Topics:
Heat transfer
,
Flow (Dynamics)
,
Blades
,
Cooling
,
Ducts
,
Heat
,
Mass transfer
,
Centrifugal force
,
Reynolds number