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Issues
January 1997
ISSN 0889-504X
EISSN 1528-8900
In this Issue
Research Papers
Flow Visualization in a Linear Turbine Cascade of High Performance Turbine Blades
J. Turbomach. January 1997, 119(1): 1–8.
doi: https://doi.org/10.1115/1.2841006
Topics:
Cascades (Fluid dynamics)
,
Flow visualization
,
Turbine blades
,
Turbines
,
Vortices
,
Blades
,
Flow (Dynamics)
,
Suction
,
Wire
,
Smoke
Transient Heat Transfer Experiments in a Linear Cascade Via an Insertion Mechanism Using the Liquid Crystal Technique
J. Turbomach. January 1997, 119(1): 9–13.
doi: https://doi.org/10.1115/1.2841016
Transient Liquid Crystal Technique for Convective Heat Transfer on Rough Surfaces
J. Turbomach. January 1997, 119(1): 14–22.
doi: https://doi.org/10.1115/1.2841004
The Influence of Large-Scale High-Intensity Turbulence on Vane Heat Transfer
J. Turbomach. January 1997, 119(1): 23–30.
doi: https://doi.org/10.1115/1.2841007
Grid Orthogonality Effects on Predicted Turbine Midspan Heat Transfer and Performance
J. Turbomach. January 1997, 119(1): 31–38.
doi: https://doi.org/10.1115/1.2841008
Topics:
Heat transfer
,
Turbines
,
Flow (Dynamics)
,
Pressure
,
Stators
Passage Flow Structure and Its Influence on Endwall Heat Transfer in a 90 deg Turning Duct: Mean Flow and High Resolution Endwall Heat Transfer Experiments
J. Turbomach. January 1997, 119(1): 39–50.
doi: https://doi.org/10.1115/1.2841009
Topics:
Ducts
,
Flow (Dynamics)
,
Heat transfer
,
Resolution (Optics)
,
Turning
,
Momentum
,
Pressure
,
Probes
,
Turbulence
,
Vorticity
Measurement and Computation of Heat Transfer in High-Pressure Compressor Drum Geometries With Axial Throughflow
J. Turbomach. January 1997, 119(1): 51–60.
doi: https://doi.org/10.1115/1.2841010
Heat Transfer From Air-Cooled Contrarotating Disks
J. Turbomach. January 1997, 119(1): 61–67.
doi: https://doi.org/10.1115/1.2841011
Topics:
Disks
,
Heat transfer
,
Computation
,
Flow (Dynamics)
,
Laser Doppler anemometry
,
Outflow
,
Reynolds number
,
Rotors
,
Stators
,
Thermocouples
Evaluation of the Interaction Losses in a Transonic Turbine HP Rotor/LP Vane Configuration
J. Turbomach. January 1997, 119(1): 68–76.
doi: https://doi.org/10.1115/1.2841012
Topics:
Rotors
,
Turbines
,
Design
,
Engineering simulation
,
Simulation
,
Wakes
,
Aircraft engines
,
Computer simulation
,
Entropy
,
Flow (Dynamics)
A Navier–Stokes Analysis of Airfoils in Oscillating Transonic Cascades for the Prediction of Aerodynamic Damping
J. Turbomach. January 1997, 119(1): 77–84.
doi: https://doi.org/10.1115/1.2841013
Topics:
Airfoils
,
Damping
,
Cascades (Fluid dynamics)
,
Compressors
,
Oscillations
,
Aeroelasticity
,
Algorithms
,
Blades
,
Flat plates
,
Flow (Dynamics)
The Influence of Neighboring Blade Rows on the Unsteady Aerodynamic Response of Cascades
J. Turbomach. January 1997, 119(1): 85–93.
doi: https://doi.org/10.1115/1.2841014
Topics:
Blades
,
Cascades (Fluid dynamics)
,
Spin (Aerodynamics)
,
Spinning (Textile)
,
Vibration
,
Waves
,
Compressors
,
Damping
,
Ducts
,
Flutter (Aerodynamics)
Three-Dimensional Unsteady Flow and Forces in Centrifugal Impellers With Circumferential Distortion of the Outlet Static Pressure
J. Turbomach. January 1997, 119(1): 94–102.
doi: https://doi.org/10.1115/1.2841015
Topics:
Impellers
,
Pressure
,
Unsteady flow
,
Acoustics
,
Boundary-value problems
,
Design
,
Flow (Dynamics)
,
Geometry
Design and Flow Field Calculations for Transonic and Supersonic Radial Inflow Turbine Guide Vanes
J. Turbomach. January 1997, 119(1): 103–113.
doi: https://doi.org/10.1115/1.2840999
Topics:
Design
,
Flow (Dynamics)
,
Guide vanes
,
Inflow
,
Turbines
,
Mach number
,
Geometry
,
Inviscid flow
,
Viscous flow
Boundary Layer Development in Axial Compressors and Turbines: Part 1 of 4—Composite Picture
J. Turbomach. January 1997, 119(1): 114–127.
doi: https://doi.org/10.1115/1.2841000
Topics:
Boundary layers
,
Composite materials
,
Compressors
,
Turbines
,
Wakes
,
Turbulence
,
Flow (Dynamics)
,
Airfoils
,
Reynolds number
,
Axial flow
Boundary Layer Development in Axial Compressors and Turbines: Part 4 of 4—Computations and Analyses
J. Turbomach. January 1997, 119(1): 128–139.
doi: https://doi.org/10.1115/1.2841001
Topics:
Boundary layers
,
Compressors
,
Computation
,
Turbines
,
Airfoils
,
Turbomachinery
Assessment of the Cold-Wire Resistance Thermometer for High-Speed Turbomachinery Applications
J. Turbomach. January 1997, 119(1): 140–148.
doi: https://doi.org/10.1115/1.2841002
Topics:
Resistance thermometers
,
Turbomachinery
,
Wire
,
Probes
,
Transfer functions
,
Heat conduction
,
Air jets
,
Atmospheric pressure
,
Frequency response
,
Heating
Performance Assessment of an Annular S-Shaped Duct
J. Turbomach. January 1997, 119(1): 149–156.
doi: https://doi.org/10.1115/1.2841003
Topics:
Ducts
,
Compressors
,
Pressure
,
Engines
,
Flow (Dynamics)
,
Shear stress
,
Struts (Engineering)
,
Aircraft
,
Blades
,
Boundary layers
Technical Briefs
Circumferentially Smeared Computed Effects of Rim Seal Clearance on Wheelspace Thermal Distributions
J. Turbomach. January 1997, 119(1): 157–159.
doi: https://doi.org/10.1115/1.2841005
Topics:
Clearances (Engineering)
,
Cavities
,
Flow (Dynamics)
,
Rotors
,
Blades
,
Computers
,
Coolants
,
Drag (Fluid dynamics)
,
Heat
,
Heating
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