Volume 114 Issue 4 | J. Turbomach. | ASME Digital Collection

Research Papers

Heat Transfer, Adiabatic Effectiveness, and Injectant Distributions Downstream of a Single Row and Two Staggered Rows of Compound Angle Film-Cooling Holes

P. M. Ligrani, S. Ciriello, D. T. Bishop

J. Turbomach. October 1992, 114(4): 687–700. doi: https://doi.org/10.1115/1.2928021

View articletitled, Heat Transfer, Adiabatic Effectiveness, and Injectant Distributions Downstream of a Single Row and Two Staggered Rows of Compound Angle Film-Cooling Holes

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Topics: Film cooling , Heat transfer , Boundary layers , Flow (Dynamics)

Discharge Coefficients of Cooling Holes With Radiused and Chamfered Inlets

N. Hay, A. Spencer

J. Turbomach. October 1992, 114(4): 701–706. doi: https://doi.org/10.1115/1.2928022

Abstract

View articletitled, Discharge Coefficients of Cooling Holes With Radiused and Chamfered Inlets

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Topics: Cooling , Discharge coefficient , Disks , Flow (Dynamics) , Gas turbines , Orifices , Performance characterization , Pressure

Influence of High Mainstream Turbulence on Leading Edge Film Cooling Heat Transfer

A. B. Mehendale, J. C. Han

J. Turbomach. October 1992, 114(4): 707–715. doi: https://doi.org/10.1115/1.2928023

Abstract

View articletitled, Influence of High Mainstream Turbulence on Leading Edge Film Cooling Heat Transfer

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Topics: Film cooling , Heat transfer , Turbulence , Heat transfer coefficients , Heat , Reynolds number , Stress

Influence of High Mainstream Turbulence on Leading Edge Film Cooling Heat Transfer: Effect of Film Hole Row Location

S. Ou, A. B. Mehendale, J. C. Han

J. Turbomach. October 1992, 114(4): 716–723. doi: https://doi.org/10.1115/1.2928024

Abstract

View articletitled, Influence of High Mainstream Turbulence on Leading Edge Film Cooling Heat Transfer: Effect of Film Hole Row Location

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Topics: Film cooling , Heat transfer , Turbulence , Heat transfer coefficients , Cylinders , Flow (Dynamics) , Heat , Reynolds number , Stress

Influence of Mainstream Turbulence on Leading Edge Film Cooling Heat Transfer Through Two Rows of Inclined Film Slots

S. Ou, J. C. Han

J. Turbomach. October 1992, 114(4): 724–733. doi: https://doi.org/10.1115/1.2928025

Abstract

View articletitled, Influence of Mainstream Turbulence on Leading Edge Film Cooling Heat Transfer Through Two Rows of Inclined Film Slots

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Topics: Film cooling , Heat transfer , Turbulence , Heat transfer coefficients , Heat , Stress , Cylinders , Flow (Dynamics) , Reynolds number

Film Cooling Research on the Endwall of a Turbine Nozzle Guide Vane in a Short Duration Annular Cascade: Part 1—Experimental Technique and Results

S. P. Harasgama, C. D. Burton

J. Turbomach. October 1992, 114(4): 734–740. doi: https://doi.org/10.1115/1.2928026

Abstract

View articletitled, Film Cooling Research on the Endwall of a Turbine Nozzle Guide Vane in a Short Duration Annular Cascade: Part 1—Experimental Technique and Results

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Topics: Cascades (Fluid dynamics) , Film cooling , Nozzle guide vanes , Turbines , Coolants , Heat transfer , Cooling , Temperature , Density , Engines

Film Cooling Research on the Endwall of a Turbine Nozzle Guide Vane in a Short Duration Annular Cascade: Part 2—Analysis and Correlation of Results

S. P. Harasgama, C. D. Burton

J. Turbomach. October 1992, 114(4): 741–746. doi: https://doi.org/10.1115/1.2928027

Abstract

View articletitled, Film Cooling Research on the Endwall of a Turbine Nozzle Guide Vane in a Short Duration Annular Cascade: Part 2—Analysis and Correlation of Results

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Topics: Cascades (Fluid dynamics) , Film cooling , Nozzle guide vanes , Turbines , Heat transfer , Pressure gradient , Cooling , Engines , Flat plates , Flow (Dynamics)

The Influence of Density Difference Between Hot and Coolant Gas on Film Cooling by a Row of Holes: Predictions and Experiments

W. Haas, W. Rodi, B. Scho¨nung

J. Turbomach. October 1992, 114(4): 747–755. doi: https://doi.org/10.1115/1.2928028

Abstract

View articletitled, The Influence of Density Difference Between Hot and Coolant Gas on Film Cooling by a Row of Holes: Predictions and Experiments

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Topics: Coolants , Density , Film cooling , Boundary layers , Flat plates , Turbine blades

Computation of a Wall Boundary Layer With Discrete Jet Injections

P. Kulisa, F. Leboeuf, G. Perrin

J. Turbomach. October 1992, 114(4): 756–764. doi: https://doi.org/10.1115/1.2928029

Abstract

View articletitled, Computation of a Wall Boundary Layer With Discrete Jet Injections

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Topics: Boundary layers , Computation , Jets , Orifices , Cooling , Flow (Dynamics) , Inviscid flow , Numerical analysis , Turbine blades

A New Hue Capturing Technique for the Quantitative Interpretation of Liquid Crystal Images Used in Convective Heat Transfer Studies

C. Camci, K. Kim, S. A. Hippensteele

J. Turbomach. October 1992, 114(4): 765–775. doi: https://doi.org/10.1115/1.2928030

Abstract

View articletitled, A New Hue Capturing Technique for the Quantitative Interpretation of Liquid Crystal Images Used in Convective Heat Transfer Studies

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Topics: Convection , Liquid crystals , Crystals , Heat transfer , Image processing , Temperature , Filters , Gas turbines , Heating , Light sources

Convective Transport Phenomena on the Suction Surface of a Turbine Blade Including the Influence of Secondary Flows Near the Endwall

P. H. Chen, R. J. Goldstein

J. Turbomach. October 1992, 114(4): 776–787. doi: https://doi.org/10.1115/1.2928031

Abstract

View articletitled, Convective Transport Phenomena on the Suction Surface of a Turbine Blade Including the Influence of Secondary Flows Near the Endwall

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Topics: Flow (Dynamics) , Suction , Transport phenomena , Turbine blades , Mass transfer , Blades , Chords (Trusses) , Heat transfer , Reynolds number , Vortices

Heat Transfer in the Turbulent Boundary Layer With a Step Change in Surface Roughness

R. P. Taylor, J. K. Taylor, H. H. Hosni, H. W. Coleman

J. Turbomach. October 1992, 114(4): 788–794. doi: https://doi.org/10.1115/1.2928032

Abstract

View articletitled, Heat Transfer in the Turbulent Boundary Layer With a Step Change in Surface Roughness

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Topics: Boundary layer turbulence , Heat transfer , Surface roughness , Turbulence , Boundary layers , Convection , Discrete element methods , Flat plates , Flow (Dynamics) , Temperature profiles

Navier–Stokes Analysis of Turbine Blade Heat Transfer and Performance

D. J. Dorney, R. L. Davis

J. Turbomach. October 1992, 114(4): 795–806. doi: https://doi.org/10.1115/1.2928033

Abstract

View articletitled, Navier–Stokes Analysis of Turbine Blade Heat Transfer and Performance

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Topics: Heat transfer , Turbine blades , Blades , Cascades (Fluid dynamics) , Density , Flow (Dynamics) , Modeling , Pressure , Turbines , Turbulence

Prediction of Unsteady Rotor-Surface Pressure and Heat Transfer From Wake Passings

L. T. Tran, D. B. Taulbee

J. Turbomach. October 1992, 114(4): 807–817. doi: https://doi.org/10.1115/1.2928034

Abstract

View articletitled, Prediction of Unsteady Rotor-Surface Pressure and Heat Transfer From Wake Passings

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Topics: Heat transfer , Pressure , Rotors , Wakes , Blades , Unsteady flow , Heat flux , Boundary layers , Inviscid flow , Boundary layer turbulence

Comparison of Time-Resolved Turbine Rotor Blade Heat Transfer Measurements and Numerical Calculations

R. S. Abhari, G. R. Guenette, A. H. Epstein, M. B. Giles

J. Turbomach. October 1992, 114(4): 818–827. doi: https://doi.org/10.1115/1.2928035

Abstract

View articletitled, Comparison of Time-Resolved Turbine Rotor Blade Heat Transfer Measurements and Numerical Calculations

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Topics: Blades , Heat transfer , Rotors , Turbines , Pressure , Algebra , Algorithms , Suction , Turbulence , Boundary layers

Film Cooling on a Gas Turbine Rotor Blade

K. Takeishi, S. Aoki, T. Sato, K. Tsukagoshi

J. Turbomach. October 1992, 114(4): 828–834. doi: https://doi.org/10.1115/1.2928036

Abstract

View articletitled, Film Cooling on a Gas Turbine Rotor Blade

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Topics: Blades , Film cooling , Gas turbines , Rotors , Rotating blades , Cascades (Fluid dynamics) , Heat , Pressure , Suction

Prediction of Turbulent Flow and Heat Transfer in a Radially Rotating Square Duct

C. Prakash, R. Zerkle

J. Turbomach. October 1992, 114(4): 835–846. doi: https://doi.org/10.1115/1.2928037

Abstract

View articletitled, Prediction of Turbulent Flow and Heat Transfer in a Radially Rotating Square Duct

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Topics: Ducts , Heat transfer , Turbulence , Buoyancy , Flow (Dynamics) , Fluids , Rotation , Temperature , Boundary-value problems , Coriolis force

Heat Transfer in Rotating Serpentine Passages With Trips Normal to the Flow

J. H. Wagner, B. V. Johnson, R. A. Graziani, F. C. Yeh

J. Turbomach. October 1992, 114(4): 847–857. doi: https://doi.org/10.1115/1.2928038

Abstract

View articletitled, Heat Transfer in Rotating Serpentine Passages With Trips Normal to the Flow

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Topics: Flow (Dynamics) , Heat transfer , Rotation , Buoyancy , Coolants , Heat transfer coefficients , Strips , Turbine blades , Cooling , Coriolis force

An Attempt to Uncouple the Effect of Coriolis and Buoyancy Forces Experimentally on Heat Transfer in Smooth Circular Tubes That Rotate in the Orthogonal Mode

W. D. Morris, R. Salemi

J. Turbomach. October 1992, 114(4): 858–864. doi: https://doi.org/10.1115/1.2928039

Abstract

View articletitled, An Attempt to Uncouple the Effect of Coriolis and Buoyancy Forces Experimentally on Heat Transfer in Smooth Circular Tubes That Rotate in the Orthogonal Mode

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Topics: Buoyancy , Heat transfer , Rotation , Convection , Coriolis force , Heat conduction , Thermal conductivity

Comparison of Heat Transfer Measurements With Computations for Turbulent Flow Around a 180 deg Bend

D. L. Besserman, S. Tanrikut

J. Turbomach. October 1992, 114(4): 865–871. doi: https://doi.org/10.1115/1.2928040

Abstract

View articletitled, Comparison of Heat Transfer Measurements With Computations for Turbulent Flow Around a 180 deg Bend

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Topics: Computation , Heat transfer , Turbulence , Fully developed turbulent flow , Airfoils , Cooling , Ducts , Durability , Flow (Dynamics) , Liquid crystals

Influence of Surface Heat Flux Ratio on Heat Transfer Augmentation in Square Channels With Parallel, Crossed, and V-Shaped Angled Ribs

J. C. Han, Y. M. Zhang, C. P. Lee

J. Turbomach. October 1992, 114(4): 872–880. doi: https://doi.org/10.1115/1.2928042

Abstract

View articletitled, Influence of Surface Heat Flux Ratio on Heat Transfer Augmentation in Square Channels With Parallel, Crossed, and V-Shaped Angled Ribs

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Topics: Heat flux , Heat transfer , Reynolds number , Heating , Copper

Computation of Laminar Flow and Heat Transfer Over an Enclosed Rotating Disk With and Without Jet Impingement

Y. Nakata, J. Y. Murthy, D. E. Metzger

J. Turbomach. October 1992, 114(4): 881–890. doi: https://doi.org/10.1115/1.2928043

Abstract

View articletitled, Computation of Laminar Flow and Heat Transfer Over an Enclosed Rotating Disk With and Without Jet Impingement

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Topics: Computation , Heat transfer , Laminar flow , Rotating disks , Disks , Cooling , Cavity flows , Convection , Flow (Dynamics) , Cavities

Hydrodynamic and Thermal Measurements in a Turbulent Boundary Layer Recovering From Concave Curvature

M. D. Kestoras, T. W. Simon

J. Turbomach. October 1992, 114(4): 891–898. doi: https://doi.org/10.1115/1.2928044

Abstract

View articletitled, Hydrodynamic and Thermal Measurements in a Turbulent Boundary Layer Recovering From Concave Curvature

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Topics: Boundary layer turbulence , Boundary layers , Curved walls , Flow (Dynamics) , Pressure gradient , Skin friction (Fluid dynamics) , Turbulence , Vortices

Research Papers

Heat Transfer, Adiabatic Effectiveness, and Injectant Distributions Downstream of a Single Row and Two Staggered Rows of Compound Angle Film-Cooling Holes

Discharge Coefficients of Cooling Holes With Radiused and Chamfered Inlets

Influence of High Mainstream Turbulence on Leading Edge Film Cooling Heat Transfer

Influence of High Mainstream Turbulence on Leading Edge Film Cooling Heat Transfer: Effect of Film Hole Row Location

Influence of Mainstream Turbulence on Leading Edge Film Cooling Heat Transfer Through Two Rows of Inclined Film Slots

Film Cooling Research on the Endwall of a Turbine Nozzle Guide Vane in a Short Duration Annular Cascade: Part 1—Experimental Technique and Results

Film Cooling Research on the Endwall of a Turbine Nozzle Guide Vane in a Short Duration Annular Cascade: Part 2—Analysis and Correlation of Results

The Influence of Density Difference Between Hot and Coolant Gas on Film Cooling by a Row of Holes: Predictions and Experiments

Computation of a Wall Boundary Layer With Discrete Jet Injections

A New Hue Capturing Technique for the Quantitative Interpretation of Liquid Crystal Images Used in Convective Heat Transfer Studies

Convective Transport Phenomena on the Suction Surface of a Turbine Blade Including the Influence of Secondary Flows Near the Endwall

Heat Transfer in the Turbulent Boundary Layer With a Step Change in Surface Roughness

Navier–Stokes Analysis of Turbine Blade Heat Transfer and Performance

Prediction of Unsteady Rotor-Surface Pressure and Heat Transfer From Wake Passings

Comparison of Time-Resolved Turbine Rotor Blade Heat Transfer Measurements and Numerical Calculations

Film Cooling on a Gas Turbine Rotor Blade

Prediction of Turbulent Flow and Heat Transfer in a Radially Rotating Square Duct

Heat Transfer in Rotating Serpentine Passages With Trips Normal to the Flow

An Attempt to Uncouple the Effect of Coriolis and Buoyancy Forces Experimentally on Heat Transfer in Smooth Circular Tubes That Rotate in the Orthogonal Mode

Comparison of Heat Transfer Measurements With Computations for Turbulent Flow Around a 180 deg Bend

Influence of Surface Heat Flux Ratio on Heat Transfer Augmentation in Square Channels With Parallel, Crossed, and V-Shaped Angled Ribs

Computation of Laminar Flow and Heat Transfer Over an Enclosed Rotating Disk With and Without Jet Impingement

Hydrodynamic and Thermal Measurements in a Turbulent Boundary Layer Recovering From Concave Curvature

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