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Issues
January 2001
ISSN 0889-504X
EISSN 1528-8900
In this Issue
Technical Papers
The Influence of Transient Inlet Distortions on the Instability Inception of a Low-Pressure Compressor in a Turbofan Engine
J. Turbomach. January 2001, 123(1): 1–8.
doi: https://doi.org/10.1115/1.1330271
Topics:
Compressors
,
Engines
,
Flow (Dynamics)
,
Pressure
,
Transients (Dynamics)
,
Sensors
,
Turbofans
,
Stall inception
,
Wavelets
Design and Test of a Semi-Passive Flow Control Device for Inlet Distortion Suppression
J. Turbomach. January 2001, 123(1): 9–13.
doi: https://doi.org/10.1115/1.1333091
Topics:
Compressors
,
Design
,
Flow (Dynamics)
,
Pressure
,
Stability
,
Surges
,
Temperature
,
Flow control
,
Compression
,
Engines
Compressor Stability Enhancement Using Discrete Tip Injection
J. Turbomach. January 2001, 123(1): 14–23.
doi: https://doi.org/10.1115/1.1330272
Topics:
Compressors
,
Ejectors
,
Flow (Dynamics)
,
Rotors
,
Stability
,
Annulus
,
Blades
,
Design
Comparative Studies on Short and Long Length-Scale Stall Cell Propagating in an Axial Compressor Rotor
J. Turbomach. January 2001, 123(1): 24–30.
doi: https://doi.org/10.1115/1.1326085
Topics:
Blades
,
Compressors
,
Flow (Dynamics)
,
Pressure
,
Rotors
,
Vortices
Identifying Faults in the Variable Geometry System of a Gas Turbine Compressor
A. Tsalavoutas, Research Assistant, K. Mathioudakis, Associate Professor, A. Stamatis, Research Associate, M. Smith, Principal Engineer,
J. Turbomach. January 2001, 123(1): 33–39.
doi: https://doi.org/10.1115/1.1330267
Topics:
Compressors
,
Engines
,
Gas turbines
,
Geometry
,
Temperature
,
Turbines
,
Guide vanes
Using Sweep and Dihedral to Control Three-Dimensional Flow in Transonic Stators of Axial Compressors
J. Turbomach. January 2001, 123(1): 40–48.
doi: https://doi.org/10.1115/1.1330268
Topics:
Airfoils
,
Blades
,
Compressors
,
Design
,
Flow (Dynamics)
,
Stators
,
Pressure
,
Boundary layers
Analysis of the Interrow Flow Field Within a Transonic Axial Compressor: Part 1—Experimental Investigation
J. Turbomach. January 2001, 123(1): 49–56.
doi: https://doi.org/10.1115/1.1328085
Topics:
Blades
,
Compressors
,
Flow (Dynamics)
,
Rotors
,
Wakes
,
Shock waves
,
Inlet guide vanes
,
Glass
,
Shock (Mechanics)
Analysis of the Interrow Flow Field Within a Transonic Axial Compressor: Part 2—Unsteady Flow Analysis
J. Turbomach. January 2001, 123(1): 57–63.
doi: https://doi.org/10.1115/1.1328086
Topics:
Blades
,
Compressors
,
Flow (Dynamics)
,
Inlet guide vanes
,
Rotors
,
Shock (Mechanics)
,
Wakes
,
Shock waves
,
Unsteady flow
,
Fluctuations (Physics)
Suppression of Rotating Stall by Wall Roughness Control in Vaneless Diffusers of Centrifugal Blowers
J. Turbomach. January 2001, 123(1): 64–72.
doi: https://doi.org/10.1115/1.1328084
Topics:
Boundary layers
,
Diffusers
,
Flow (Dynamics)
,
Pressure
,
Separation (Technology)
,
Surface roughness
,
Vaneless diffusers
,
Friction
,
Impellers
Direct Method for Optimization of a Centrifugal Compressor Vaneless Diffuser
J. Turbomach. January 2001, 123(1): 73–79.
doi: https://doi.org/10.1115/1.1308571
Topics:
Compressors
,
Diffusers
,
Optimization
,
Vaneless diffusers
,
Turbulence
,
Design
,
Shapes
,
Pressure
,
Reynolds-averaged Navier–Stokes equations
Investigation of the Unsteady Rotor Aerodynamics in a Transonic Turbine Stage
J. Turbomach. January 2001, 123(1): 81–89.
doi: https://doi.org/10.1115/1.1314607
Topics:
Blades
,
Pressure
,
Rotors
,
Shock (Mechanics)
,
Stators
,
Turbines
,
Wakes
,
Flow (Dynamics)
,
Computation
,
Fluctuations (Physics)
Experimental Heat Transfer and Bulk Air Temperature Measurements for a Multipass Internal Cooling Model With Ribs and Bleed
J. Turbomach. January 2001, 123(1): 90–96.
doi: https://doi.org/10.1115/1.1333090
Topics:
Cooling
,
Heat transfer
,
Temperature
,
Temperature measurement
,
Flow (Dynamics)
,
Liquid crystals
Heat Transfer Enhancements in Rotating Two-Pass Coolant Channels With Profiled Ribs: Part 1–Average Results
J. Turbomach. January 2001, 123(1): 97–106.
doi: https://doi.org/10.1115/1.1331539
Topics:
Coolants
,
Ducts
,
Flow (Dynamics)
,
Heat transfer
,
Mass transfer
,
Gas turbines
Heat Transfer Enhancements in Rotating Two-Pass Coolant Channels With Profiled Ribs: Part 2—Detailed Measurements
J. Turbomach. January 2001, 123(1): 107–114.
doi: https://doi.org/10.1115/1.1331538
Topics:
Coolants
,
Ducts
,
Flow (Dynamics)
,
Heat transfer
,
Mass transfer
,
Rotation
,
Reynolds number
,
Gas turbines
Local Heat Transfer and Flow Structure on and Above a Dimpled Surface in a Channel
G. I. Mahmood, Graduate Student, M. L. Hill, Graduate Student, D. L. Nelson, Graduate Student, P. M. Ligrani, Professor., H.-K. Moon, Consulting Engineer, B. Glezer, Head, Turbine Cooling and Heat Transfer Analysis
J. Turbomach. January 2001, 123(1): 115–123.
doi: https://doi.org/10.1115/1.1333694
Topics:
Flow (Dynamics)
,
Flow visualization
,
Heat transfer
,
Pressure
,
Reynolds number
,
Temperature
,
Vortices
,
Fluids
Flow and Heat Transfer in a Rotating Square Channel With 45 deg Angled Ribs by Reynolds Stress Turbulence Model
J. Turbomach. January 2001, 123(1): 124–132.
doi: https://doi.org/10.1115/1.1333092
Topics:
Flow (Dynamics)
,
Heat transfer
,
Stress
,
Turbulence
,
Rotation
,
Ducts
,
Coriolis force
,
Temperature
,
Coolants
Lateral-Flow Effect on Endwall Heat Transfer and Pressure Drop in a Pin-Fin Trapezoidal Duct of Various Pin Shapes
J. Turbomach. January 2001, 123(1): 133–139.
doi: https://doi.org/10.1115/1.1333093
Topics:
Ducts
,
Flow (Dynamics)
,
Heat transfer
,
Pressure drop
,
Shapes
,
Heat transfer coefficients
,
Pins (Engineering)
,
Reynolds number
Augmentation of Stagnation Region Heat Transfer Due to Turbulence From a DLN Can Combustor
J. Turbomach. January 2001, 123(1): 140–146.
doi: https://doi.org/10.1115/1.1330270
Topics:
Combustion chambers
,
Flow (Dynamics)
,
Heat transfer
,
Turbulence
,
Wire
,
Probes
An Experimental Evaluation of Advanced Leading Edge Impingement Cooling Concepts
J. Turbomach. January 2001, 123(1): 147–153.
doi: https://doi.org/10.1115/1.1331537
Topics:
Cooling
,
Flow (Dynamics)
,
Geometry
,
Heat transfer
,
Heat transfer coefficients
,
Jets
,
Surface roughness
,
Airfoils
,
Reynolds number
,
Convection
Heat Transfer and Flow Characteristics of an Engine Representative Impingement Cooling System
J. Turbomach. January 2001, 123(1): 154–160.
doi: https://doi.org/10.1115/1.1328087
Mist/Steam Heat Transfer in Confined Slot Jet Impingement
J. Turbomach. January 2001, 123(1): 161–167.
doi: https://doi.org/10.1115/1.1331536
Topics:
Drops
,
Flow (Dynamics)
,
Heat transfer
,
Steam
,
Cooling
Infrared Low-Temperature Turbine Vane Rough Surface Heat Transfer Measurements
J. Turbomach. January 2001, 123(1): 168–177.
doi: https://doi.org/10.1115/1.1333693
Topics:
Heat transfer
,
Surface roughness
,
Temperature
,
Turbulence
,
Turbines
,
Suction
,
Reynolds number
,
Mach number
,
Pressure
,
Flow (Dynamics)
Discussion: “Comparative Studies on Short and Long Length-Scale Stall Cell Propagating in an Axial Compressor Rotor” (Inoue, M., Kuroumaru, M., Tanino, T., Yoshida, S., and Furukawa, M., 2001, ASME J. Turbomach., 123, pp. 24–30)
J. Turbomach. January 2001, 123(1): 31.
doi: https://doi.org/10.1115/1.1326084
Topics:
Compressors
,
Rotors
,
Vortices
,
Aerodynamics
,
Fluctuations (Physics)
,
Pressure measurement
,
Rotational flow
Closure to “Discussion of ‘Comparative Studies on Short and Long Length-Scale Stall Cell Propagating in an Axial Compressor Rotor’ ” (2001, ASME J. Turbomach., 123, p. 31)
J. Turbomach. January 2001, 123(1): 31–32.
doi: https://doi.org/10.1115/1.1332393
Topics:
Compressors
,
Rotors
,
Vortices
,
Aerodynamics
,
Rotational flow
Discussion: “Direct Method for Optimization of a Centrifugal Compressor Vaneless Diffuser” (Lee, Y.-T., Luo, L., and Bein, T. W., 2001, ASME J. Turbomach., 123, pp. 73–79)
J. Turbomach. January 2001, 123(1): 79–80.
doi: https://doi.org/10.1115/1.1324666
Topics:
Compressors
,
Optimization
,
Vaneless diffusers
,
Fluid dynamics
,
Stagnation flow
,
Turbulence
Closure to “Discussion of ‘Direction Method for Optimization of a Centrifugal Compressor Vaneless Diffuser’ ” (2000, ASME, J. Turbomach., 123, p. 79)
J. Turbomach. January 2001, 123(1): 80.
doi: https://doi.org/10.1115/1.1333089
Topics:
Compressors
,
Optimization
,
Fluid dynamics
,
Stagnation flow
,
Turbulence
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The Cooling Effect of Combustor Exit Louver Scheme on a Transonic Nozzle Guide Vane Endwall
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