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Issues
October 2001
ISSN 0889-504X
EISSN 1528-8900
In this Issue
Technical Papers
Convective Heat Transfer and Aerodynamics in Axial Flow Turbines
J. Turbomach. October 2001, 123(4): 637–686.
doi: https://doi.org/10.1115/1.1397776
Topics:
Blades
,
Heat transfer
,
Pressure
,
Turbines
,
Turbulence
,
Flow (Dynamics)
,
Film cooling
Mainstream Aerodynamic Effects Due to Wheelspace Coolant Injection in a High-Pressure Turbine Stage: Part I—Aerodynamic Measurements in the Stationary Frame
J. Turbomach. October 2001, 123(4): 687–696.
doi: https://doi.org/10.1115/1.1401026
Topics:
Coolants
,
Cooling
,
Flow (Dynamics)
,
Pressure
,
Rotors
,
Turbines
,
Uncertainty
,
Impingement cooling
,
High pressure (Physics)
Mainstream Aerodynamic Effects Due to Wheelspace Coolant Injection in a High-Pressure Turbine Stage: Part II—Aerodynamic Measurements in the Rotational Frame
J. Turbomach. October 2001, 123(4): 697–703.
doi: https://doi.org/10.1115/1.1397303
Topics:
Coolants
,
Cooling
,
Flow (Dynamics)
,
High pressure (Physics)
,
Pressure
,
Rotors
,
Turbines
,
Wakes
,
Impingement cooling
,
Probes
Heat Transfer and Flow on the Blade Tip of a Gas Turbine Equipped With a Mean-Camberline Strip
J. Turbomach. October 2001, 123(4): 704–708.
doi: https://doi.org/10.1115/1.1400114
Topics:
Blades
,
Flow (Dynamics)
,
Heat transfer
,
Strips
,
Leakage
,
Gas turbines
,
Geometry
Film-Cooled Turbine Endwall in a Transonic Flow Field: Part I—Aerodynamic Measurements
J. Turbomach. October 2001, 123(4): 709–719.
doi: https://doi.org/10.1115/1.1400112
Topics:
Coolants
,
Flow (Dynamics)
,
Pressure
Film-Cooled Turbine Endwall in a Transonic Flow Field: Part II—Heat Transfer and Film-Cooling Effectiveness
J. Turbomach. October 2001, 123(4): 720–729.
doi: https://doi.org/10.1115/1.1397308
Topics:
Coolants
,
Film cooling
,
Flow (Dynamics)
,
Heat transfer
,
Cooling
,
Turbines
,
Heat transfer coefficients
,
Temperature
Turbine Nozzle Endwall Film Cooling Study Using Pressure-Sensitive Paint
J. Turbomach. October 2001, 123(4): 730–738.
doi: https://doi.org/10.1115/1.1400113
Topics:
Cooling
,
Film cooling
,
Flow (Dynamics)
,
Nozzles
,
Pressure
,
Turbines
,
Nitrogen
,
Paints
,
Oxygen
,
Turbulence
The Many Faces of Turbine Surface Roughness
J. Turbomach. October 2001, 123(4): 739–748.
doi: https://doi.org/10.1115/1.1400115
Topics:
Surface roughness
,
Turbines
,
Spallation (Nuclear physics)
High-Resolution Measurements of Local Heat Transfer Coefficients From Discrete Hole Film Cooling
J. Turbomach. October 2001, 123(4): 749–757.
doi: https://doi.org/10.1115/1.1387245
Topics:
Coolants
,
Density
,
Film cooling
,
Flow (Dynamics)
,
Heat flux
,
Heat transfer
,
Heat transfer coefficients
,
Resolution (Optics)
,
Temperature
,
Vortices
High-Resolution Measurements of Local Effectiveness From Discrete Hole Film Cooling
J. Turbomach. October 2001, 123(4): 758–765.
doi: https://doi.org/10.1115/1.1371778
Topics:
Coolants
,
Cooling
,
Density
,
Film cooling
,
Finite element analysis
,
Flow (Dynamics)
,
Heat flux
,
Jets
,
Momentum
,
Resolution (Optics)
An Experimental Study of Impingement on Roughened Airfoil Leading-Edge Walls With Film Holes
J. Turbomach. October 2001, 123(4): 766–773.
doi: https://doi.org/10.1115/1.1401035
Topics:
Airfoils
,
Flow (Dynamics)
,
Geometry
,
Heat transfer
,
Heat transfer coefficients
,
Reynolds number
,
Cooling
,
Pressure
,
Jets
Film Cooling Discharge Coefficient Measurements in a Turbulated Passage With Internal Crossflow
J. Turbomach. October 2001, 123(4): 774–780.
doi: https://doi.org/10.1115/1.1397307
Topics:
Discharge coefficient
,
Flow (Dynamics)
,
Pressure
,
Film cooling
Effect of Crossflows on the Discharge Coefficient of Film Cooling Holes With Varying Angles of Inclination and Orientation
J. Turbomach. October 2001, 123(4): 781–787.
doi: https://doi.org/10.1115/1.1397306
Topics:
Discharge coefficient
,
Film cooling
,
Mach number
,
Pressure
,
Flow (Dynamics)
Shock Wave–Film Cooling Interactions in Transonic Flows
J. Turbomach. October 2001, 123(4): 788–797.
doi: https://doi.org/10.1115/1.1397305
Topics:
Film cooling
,
Mach number
,
Shock waves
,
Flow (Dynamics)
Full-Coverage Film Cooling With Short Normal Injection Holes
J. Turbomach. October 2001, 123(4): 798–805.
doi: https://doi.org/10.1115/1.1400111
Topics:
Coolants
,
Film cooling
,
Turbulence
,
Jets
Heat/Mass Transfer Measurement Within a Film Cooling Hole of Square and Rectangular Cross Section
J. Turbomach. October 2001, 123(4): 806–814.
doi: https://doi.org/10.1115/1.1400109
Topics:
Film cooling
,
Flow (Dynamics)
,
Heat
,
Mass transfer
,
Reynolds number
,
Vortices
Effects of Reynolds Number and Pressure Ratio on Leakage Loss and Heat Transfer in a Stepped Labyrinth Seal
J. Turbomach. October 2001, 123(4): 815–822.
doi: https://doi.org/10.1115/1.1397304
Topics:
Discharge coefficient
,
Heat transfer
,
Leakage
,
Pressure
,
Reynolds number
,
Flow (Dynamics)
,
Geometry
,
Stators
The Application of Pressure- and Temperature-Sensitive Paints to an Advanced Compressor
J. Turbomach. October 2001, 123(4): 823–829.
doi: https://doi.org/10.1115/1.1400116
Topics:
Compressors
,
Paints
,
Pressure
,
Temperature
,
Computational fluid dynamics
,
Pressure measurement
,
Blades
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