Volume 110 Issue 1 | J. Turbomach. | ASME Digital Collection

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Volume 110, Issue 1

January 1988

ISSN 0889-504X

EISSN 1528-8900

Research Papers

Growth of Secondary Losses and Vorticity in an Axial Turbine Cascade

D. G. Gregory-Smith, C. P. Graves, J. A. Walsh

J. Turbomach. January 1988, 110(1): 1–8. doi: https://doi.org/10.1115/1.3262163

Abstract

View articletitled, Growth of Secondary Losses and Vorticity in an Axial Turbine Cascade

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Topics: Cascades (Fluid dynamics) , Turbines , Vorticity , Flow (Dynamics) , Blades , Flow visualization , Kinetic energy , Rotors , Separation (Technology) , Vortices

The Base Pressure and Loss of a Family of Four Turbine Blades

L. Xu, J. D. Denton

J. Turbomach. January 1988, 110(1): 9–17. doi: https://doi.org/10.1115/1.3262174

Abstract

View articletitled, The Base Pressure and Loss of a Family of Four Turbine Blades

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Topics: Pressure , Turbine blades , Blades , Geometry , Mach number , Turbines

Tip Leakage Flow in a Linear Turbine Cascade

J. Moore, J. S. Tilton

J. Turbomach. January 1988, 110(1): 18–26. doi: https://doi.org/10.1115/1.3262162

Abstract

View articletitled, Tip Leakage Flow in a Linear Turbine Cascade

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Topics: Cascades (Fluid dynamics) , Leakage flows , Turbines , Flow (Dynamics) , Blades , Pressure , Heat transfer , Rotors , Clearances (Engineering) , Errors

Modeling the Unsteady Flow in a Turbine Rotor Passage

D. J. Doorly

J. Turbomach. January 1988, 110(1): 27–37. doi: https://doi.org/10.1115/1.3262164

Abstract

View articletitled, Modeling the Unsteady Flow in a Turbine Rotor Passage

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Topics: Modeling , Rotors , Turbines , Unsteady flow , Wakes , Boundary layers , Blades , Heat flux , Turbulence , Reynolds number

A Trace Gas Technique to Study Mixing in a Turbine Stage

H. D. Joslyn, R. P. Dring

J. Turbomach. January 1988, 110(1): 38–43. doi: https://doi.org/10.1115/1.3262165

Abstract

View articletitled, A Trace Gas Technique to Study Mixing in a Turbine Stage

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Topics: Turbines , Stators , Temperature profiles , Airfoils , Axial flow , Diffusion (Physics) , Flow (Dynamics) , Flow visualization , Rotors , Temperature

The Influence of Rotation on the Heat Transfer Characteristics of Circular, Triangular, and Square-Sectioned Coolant Passages of Gas Turbine Rotor Blades

S. P. Harasgama, W. D. Morris

J. Turbomach. January 1988, 110(1): 44–50. doi: https://doi.org/10.1115/1.3262166

Abstract

View articletitled, The Influence of Rotation on the Heat Transfer Characteristics of Circular, Triangular, and Square-Sectioned Coolant Passages of Gas Turbine Rotor Blades

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Topics: Blades , Coolants , Gas turbines , Heat transfer , Rotation , Rotors , Flow (Dynamics) , Buoyancy , Ducts , Cooling

Time-Averaged Heat-Flux Distributions and Comparison With Prediction for the Teledyne 702 HP Turbine Stage

M. G. Dunn, R. E. Chupp

J. Turbomach. January 1988, 110(1): 51–56. doi: https://doi.org/10.1115/1.3262167

Abstract

View articletitled, Time-Averaged Heat-Flux Distributions and Comparison With Prediction for the Teledyne 702 HP Turbine Stage

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Topics: Heat flux , Turbines , Blades , Turbulence , Flat plates , Gages , Pressure , Thin films , Computer-aided engineering , Eddies (Fluid dynamics)

Film Cooling and Heat Transfer in Nozzles

J. Stoll, J. Straub

J. Turbomach. January 1988, 110(1): 57–65. doi: https://doi.org/10.1115/1.3262168

Abstract

View articletitled, Film Cooling and Heat Transfer in Nozzles

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Topics: Film cooling , Heat transfer , Nozzles , Heat flux , Boundary layers , Compressed air , Cooling , Pressure gradient , Stability , Turbulence

Stagnation Film Cooling and Heat Transfer, Including Its Effect Within the Hole Pattern

W. J. Mick, R. E. Mayle

J. Turbomach. January 1988, 110(1): 66–72. doi: https://doi.org/10.1115/1.3262169

Abstract

View articletitled, Stagnation Film Cooling and Heat Transfer, Including Its Effect Within the Hole Pattern

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Topics: Film cooling , Heat transfer , Heat transfer coefficients , Flow (Dynamics) , Heat , Stress , Cooling , Temperature , Turbines

Turbulence Measurements in Turbine Blade Passages and Implications for Heat Transfer

W. J. Priddy, F. J. Bayley

J. Turbomach. January 1988, 110(1): 73–79. doi: https://doi.org/10.1115/1.3262170

Abstract

View articletitled, Turbulence Measurements in Turbine Blade Passages and Implications for Heat Transfer

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Topics: Heat transfer , Turbine blades , Turbulence , Flow (Dynamics) , Lasers , Blades , Cascades (Fluid dynamics) , Convection , Engineering simulation , Engines

Measurements of the Turbulent Transport of Heat and Momentum in Convexly Curved Boundary Layers: Effects of Curvature, Recovery and Free-Stream Turbulence

J. Kim, T. W. Simon

J. Turbomach. January 1988, 110(1): 80–87. doi: https://doi.org/10.1115/1.3262171

Abstract

View articletitled, Measurements of the Turbulent Transport of Heat and Momentum in Convexly Curved Boundary Layers: Effects of Curvature, Recovery and Free-Stream Turbulence

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Topics: Boundary layers , Heat , Momentum , Turbulence , Wire , Boundary layer turbulence , Prandtl number , Probes

A Study of the Effects of Thermal Barrier Coating Surface Roughness on the Boundary Layer Characteristics of Gas Turbine Aerofoils

R. M. Watt, J. L. Allen, N. C. Baines, J. P. Simons, M. George

J. Turbomach. January 1988, 110(1): 88–93. doi: https://doi.org/10.1115/1.3262172

Abstract

View articletitled, A Study of the Effects of Thermal Barrier Coating Surface Roughness on the Boundary Layer Characteristics of Gas Turbine Aerofoils

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Topics: Airfoils , Boundary layers , Gas turbines , Surface roughness , Thermal barrier coatings , Cascades (Fluid dynamics) , Reynolds number , Design , Nozzle guide vanes , Polishing

A Review of Staggered Array Pin Fin Heat Transfer for Turbine Cooling Applications

J. Armstrong, D. Winstanley

J. Turbomach. January 1988, 110(1): 94–103. doi: https://doi.org/10.1115/1.3262173

Abstract

View articletitled, A Review of Staggered Array Pin Fin Heat Transfer for Turbine Cooling Applications

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Topics: Cooling , Heat transfer , Turbines , Flow (Dynamics) , Friction , Fins

Aerodynamic Design of a Power Turbine for an Aircraft Derivative Marine Gas Turbine

Guiming Ji, Zengxiang Tan, Mingchang Zhang

J. Turbomach. January 1988, 110(1): 104–109. doi: https://doi.org/10.1115/1.3262154

Abstract

View articletitled, Aerodynamic Design of a Power Turbine for an Aircraft Derivative Marine Gas Turbine

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Topics: Aircraft , Design , Marine gas turbines , Turbines , Equilibrium (Physics) , Blades , Design methodology , Flow (Dynamics) , Generators , Geometry

Performance Characteristics of Two- and Three-Dimensional Impellers in Centrifugal Compressors

H. Harada

J. Turbomach. January 1988, 110(1): 110–114. doi: https://doi.org/10.1115/1.3262155

Abstract

View articletitled, Performance Characteristics of Two- and Three-Dimensional Impellers in Centrifugal Compressors

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Topics: Compressors , Impellers , Performance characterization , Blades , Fluids , Probes

Analysis of Measurements in Vaned Diffusers of Centrifugal Compressors

W. Stein, M. Rautenberg

J. Turbomach. January 1988, 110(1): 115–121. doi: https://doi.org/10.1115/1.3262156

Abstract

View articletitled, Analysis of Measurements in Vaned Diffusers of Centrifugal Compressors

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Topics: Compressors , Diffusers , Flow (Dynamics) , Geometry , Computational methods

Swirling Impeller Flow

H. Krain

J. Turbomach. January 1988, 110(1): 122–128. doi: https://doi.org/10.1115/1.3262157

Abstract

View articletitled, Swirling Impeller Flow

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Topics: Flow (Dynamics) , Impellers , Swirling flow , Rotors , Blades , Lasers , Vortex flow , Wakes

Blade Excitation by Broad-Band Pressure Fluctuations in a Centrifugal Compressor

U. Haupt, M. Rautenberg, A. N. Abdel-Hamid

J. Turbomach. January 1988, 110(1): 129–137. doi: https://doi.org/10.1115/1.3262158

Abstract

View articletitled, Blade Excitation by Broad-Band Pressure Fluctuations in a Centrifugal Compressor

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Topics: Blades , Compressors , Excitation , Fluctuations (Physics) , Pressure , Flow (Dynamics) , Impellers , Vibration , Design , Diffusers

The Measurement of Boundary Layers on a Compressor Blade in Cascade: Part 2—Suction Surface Boundary Layers

S. Deutsch, W. C. Zierke

J. Turbomach. January 1988, 110(1): 138–145. doi: https://doi.org/10.1115/1.3262159

Abstract

View articletitled, The Measurement of Boundary Layers on a Compressor Blade in Cascade: Part 2—Suction Surface Boundary Layers

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Topics: Blades , Boundary layers , Cascades (Fluid dynamics) , Compressors , Suction , Chords (Trusses) , Separation (Technology) , Boundary layer turbulence , Bubbles , Flow visualization

The Measurement of Boundary Layers on a Compressor Blade in Cascade: Part 3—Pressure Surface Boundary Layers and the Near Wake

S. Deutsch, W. C. Zierke

J. Turbomach. January 1988, 110(1): 146–152. doi: https://doi.org/10.1115/1.3262160

Abstract

View articletitled, The Measurement of Boundary Layers on a Compressor Blade in Cascade: Part 3—Pressure Surface Boundary Layers and the Near Wake

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Topics: Blades , Boundary layers , Cascades (Fluid dynamics) , Compressors , Pressure , Wakes , Chords (Trusses) , Turbulence , Errors , Flow visualization

Technical Briefs

A Note on Spanwise Mixing

P. W. James

J. Turbomach. January 1988, 110(1): 153–154. doi: https://doi.org/10.1115/1.3262161

View articletitled, A Note on Spanwise Mixing

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Research Papers

Growth of Secondary Losses and Vorticity in an Axial Turbine Cascade

The Base Pressure and Loss of a Family of Four Turbine Blades

Tip Leakage Flow in a Linear Turbine Cascade

Modeling the Unsteady Flow in a Turbine Rotor Passage

A Trace Gas Technique to Study Mixing in a Turbine Stage

The Influence of Rotation on the Heat Transfer Characteristics of Circular, Triangular, and Square-Sectioned Coolant Passages of Gas Turbine Rotor Blades

Time-Averaged Heat-Flux Distributions and Comparison With Prediction for the Teledyne 702 HP Turbine Stage

Film Cooling and Heat Transfer in Nozzles

Stagnation Film Cooling and Heat Transfer, Including Its Effect Within the Hole Pattern

Turbulence Measurements in Turbine Blade Passages and Implications for Heat Transfer

Measurements of the Turbulent Transport of Heat and Momentum in Convexly Curved Boundary Layers: Effects of Curvature, Recovery and Free-Stream Turbulence

A Study of the Effects of Thermal Barrier Coating Surface Roughness on the Boundary Layer Characteristics of Gas Turbine Aerofoils

A Review of Staggered Array Pin Fin Heat Transfer for Turbine Cooling Applications

Aerodynamic Design of a Power Turbine for an Aircraft Derivative Marine Gas Turbine

Performance Characteristics of Two- and Three-Dimensional Impellers in Centrifugal Compressors

Analysis of Measurements in Vaned Diffusers of Centrifugal Compressors

Swirling Impeller Flow

Blade Excitation by Broad-Band Pressure Fluctuations in a Centrifugal Compressor

The Measurement of Boundary Layers on a Compressor Blade in Cascade: Part 2—Suction Surface Boundary Layers

The Measurement of Boundary Layers on a Compressor Blade in Cascade: Part 3—Pressure Surface Boundary Layers and the Near Wake

Technical Briefs

A Note on Spanwise Mixing

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