Volume 108 Issue 1 | J. Turbomach. | ASME Digital Collection

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Volume 108, Issue 1

July 1986

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ISSN 0889-504X

EISSN 1528-8900

Editorial

Arthur J. Wennerstrom

J. Turbomach. July 1986, 108(1): 1. doi: https://doi.org/10.1115/1.3262017

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Research Papers

Spanwise Mixing in Multistage Axial Flow Compressors: Part I—Experimental Investigation

S. J. Gallimore, N. A. Cumpsty

J. Turbomach. July 1986, 108(1): 2–9. doi: https://doi.org/10.1115/1.3262019

Abstract

View articletitled, Spanwise Mixing in Multistage Axial Flow Compressors: Part I—Experimental Investigation

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Topics: Axial flow , Compressors , Aerodynamics , Convection , Diffusion (Physics) , Flow (Dynamics) , Machinery , Turbulence , Wake turbulence

Spanwise Mixing in Multistage Axial Flow Compressors: Part II—Throughflow Calculations Including Mixing

S. J. Gallimore

J. Turbomach. July 1986, 108(1): 10–16. doi: https://doi.org/10.1115/1.3262009

Abstract

View articletitled, Spanwise Mixing in Multistage Axial Flow Compressors: Part II—Throughflow Calculations Including Mixing

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Topics: Axial flow , Compressors , Flow (Dynamics) , Machinery , Temperature , Turbulent diffusion

Through-Flow Analysis of a Multistage Compressor: Part I—Aerodynamic Input

R. P. Dring, H. D. Joslyn

J. Turbomach. July 1986, 108(1): 17–22. doi: https://doi.org/10.1115/1.3262016

Abstract

View articletitled, Through-Flow Analysis of a Multistage Compressor: Part I—Aerodynamic Input

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Topics: Compressors , Flow (Dynamics) , Airfoils , Databases , Design , Mach number , Rotors , Stators , Turbomachinery

Through-Flow Analysis of a Multistage Compressor: Part II—Analytical-Experimental Comparisons

R. P. Dring, H. D. Joslyn

J. Turbomach. July 1986, 108(1): 23–31. doi: https://doi.org/10.1115/1.3262018

Abstract

View articletitled, Through-Flow Analysis of a Multistage Compressor: Part II—Analytical-Experimental Comparisons

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Topics: Compressors , Flow (Dynamics) , Airfoils , Design , Mach number , Rotors , Stators , Turbomachinery

The Development of a Second Generation of Controlled Diffusion Airfoils for Multistage Compressors

R. F. Behlke

J. Turbomach. July 1986, 108(1): 32–40. doi: https://doi.org/10.1115/1.3262020

Abstract

View articletitled, The Development of a Second Generation of Controlled Diffusion Airfoils for Multistage Compressors

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Topics: Airfoils , Compressors , Diffusion (Physics) , Design , Blades , Cascades (Fluid dynamics) , Engines , Flow (Dynamics) , Mach number , Surges

Comparison of Calculated and Experimental Cascade Performance for Controlled-Diffusion Compressor Stator Blading

N. L. Sanger, R. P. Shreeve

J. Turbomach. July 1986, 108(1): 42–50. doi: https://doi.org/10.1115/1.3262023

Abstract

View articletitled, Comparison of Calculated and Experimental Cascade Performance for Controlled-Diffusion Compressor Stator Blading

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Topics: Cascades (Fluid dynamics) , Compressors , Diffusion (Physics) , Stators , Blades , Chords (Trusses) , Boundary layers , Computation , Inviscid flow , Reynolds number

Study of Three-Dimensional Viscous Flows in an Axial Compressor Cascade Including Tip Leakage Effects Using a SIMPLE-Based Algorithm

M. Pouagare, R. A. Delaney

J. Turbomach. July 1986, 108(1): 51–58. doi: https://doi.org/10.1115/1.3262024

Abstract

View articletitled, Study of Three-Dimensional Viscous Flows in an Axial Compressor Cascade Including Tip Leakage Effects Using a SIMPLE-Based Algorithm

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Topics: Algorithms , Cascades (Fluid dynamics) , Compressors , Flow (Dynamics) , Leakage , Computer simulation , Leakage flows , Separation (Technology) , Vortices , Clearances (Engineering)

On the Application of a Linearized Unsteady Potential-Flow Analysis to Fan-Tip Cascades

W. J. Usab, Jr., J. M. Verdon

J. Turbomach. July 1986, 108(1): 59–67. doi: https://doi.org/10.1115/1.3262025

Abstract

View articletitled, On the Application of a Linearized Unsteady Potential-Flow Analysis to Fan-Tip Cascades

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Topics: Flow (Dynamics) , Blades , Cascades (Fluid dynamics) , Airfoils , Flat plates , Geometry , Mach number , NASA

Computation of Inviscid Incompressible Flow Using the Primitive Variable Formulation

S. Abdallah, H. G. Smith

J. Turbomach. July 1986, 108(1): 68–75. doi: https://doi.org/10.1115/1.3262026

Abstract

View articletitled, Computation of Inviscid Incompressible Flow Using the Primitive Variable Formulation

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Topics: Computation , Flow (Dynamics) , Pressure , Boundary-value problems , Momentum , Ducts , Navier-Stokes equations , Poisson equation , Rotational flow , Theorems (Mathematics)

Performance of Axial Compressor With Nonuniform Exit Static Pressure

H. Kodama

J. Turbomach. July 1986, 108(1): 76–81. doi: https://doi.org/10.1115/1.3262027

Abstract

View articletitled, Performance of Axial Compressor With Nonuniform Exit Static Pressure

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Topics: Compressors , Pressure , Actuators , Disks , Fans

Predictive Surge Control and Optimization for a Centrifugal Compressor

D. Patlovany, A. B. Focke

J. Turbomach. July 1986, 108(1): 82–89. doi: https://doi.org/10.1115/1.3262028

Abstract

View articletitled, Predictive Surge Control and Optimization for a Centrifugal Compressor

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Topics: Compressors , Optimization , Surges , Control systems , Air compressors , Damage , Energy consumption

Heat-Flux Measurements for the Rotor of a Full-Stage Turbine: Part I—Time-Averaged Results

M. G. Dunn

J. Turbomach. July 1986, 108(1): 90–97. doi: https://doi.org/10.1115/1.3262029

Abstract

View articletitled, Heat-Flux Measurements for the Rotor of a Full-Stage Turbine: Part I—Time-Averaged Results

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Topics: Heat flux , Rotors , Turbine components , Blades , Flat plates , Pressure , Nozzle guide vanes , Suction , Turbines , Turbulence

Heat-Flux Measurements for the Rotor of a Full-Stage Turbine: Part II—Description of Analysis Technique and Typical Time-Resolved Measurements

M. G. Dunn, W. K. George, W. J. Rae, S. H. Woodward, J. C. Moller, P. J. Seymour

J. Turbomach. July 1986, 108(1): 98–107. doi: https://doi.org/10.1115/1.3262030

Abstract

View articletitled, Heat-Flux Measurements for the Rotor of a Full-Stage Turbine: Part II—Description of Analysis Technique and Typical Time-Resolved Measurements

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Topics: Heat flux , Rotors , Turbine components , Blades , Gages , Suction , Thin films , Turbines , Cutting , Data acquisition

Heat-Flux and Pressure Measurements and Comparison With Prediction for a Low-Aspect-Ratio Turbine Stage

M. G. Dunn, H. L. Martin, M. J. Stanek

J. Turbomach. July 1986, 108(1): 108–115. doi: https://doi.org/10.1115/1.3262008

Abstract

View articletitled, Heat-Flux and Pressure Measurements and Comparison With Prediction for a Low-Aspect-Ratio Turbine Stage

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Topics: Heat flux , Pressure measurement , Turbines , Nozzle guide vanes , Gages , Pressure , Airfoils , Blades , Flat plates , Shock tubes

Laminar and Transitional Boundary Layer Structures in Accelerating Flow With Heat Transfer

K. Rued, S. Wittig

J. Turbomach. July 1986, 108(1): 116–123. doi: https://doi.org/10.1115/1.3262010

Abstract

View articletitled, Laminar and Transitional Boundary Layer Structures in Accelerating Flow With Heat Transfer

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Topics: Boundary layers , Flow (Dynamics) , Heat transfer , Gas turbines , Blades , Cooling , Flat plates , Heat transfer coefficients , Pressure gradient , Turbines

Systematic Study of Film Cooling With a Three-Dimensional Calculation Procedure

A. O. Demuren, W. Rodi, B. Scho¨nung

J. Turbomach. July 1986, 108(1): 124–130. doi: https://doi.org/10.1115/1.3262011

Abstract

View articletitled, Systematic Study of Film Cooling With a Three-Dimensional Calculation Procedure

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Topics: Film cooling , Cooling , Eddies (Fluid dynamics) , Finite volume methods , Flux (Metallurgy) , Heat , Stress , Temperature distribution , Turbulence , Viscosity

Heat Transfer Downstream of a Leading Edge Separation Bubble

W. J. Bellows, R. E. Mayle

J. Turbomach. July 1986, 108(1): 131–136. doi: https://doi.org/10.1115/1.3262012

Abstract

View articletitled, Heat Transfer Downstream of a Leading Edge Separation Bubble

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Topics: Bubbles , Heat transfer , Separation (Technology) , Boundary layer turbulence , Boundary layers , Flat plates , Flow (Dynamics) , Momentum , Reynolds number , Turbulence

Flat-Plate Film Cooling With Steam Injection Through One Row and Two Rows of Inclined Holes

J. C. Han, A. B. Mehendale

J. Turbomach. July 1986, 108(1): 137–144. doi: https://doi.org/10.1115/1.3262013

Abstract

View articletitled, Flat-Plate Film Cooling With Steam Injection Through One Row and Two Rows of Inclined Holes

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Topics: Film cooling , Flat plates , Steam

The Effect of Inlet Conditions on Heat Transfer in a Rotating Cavity With a Radial Outflow of Fluid

C. A. Long, J. M. Owen

J. Turbomach. July 1986, 108(1): 145–152. doi: https://doi.org/10.1115/1.3262014

Abstract

View articletitled, The Effect of Inlet Conditions on Heat Transfer in a Rotating Cavity With a Radial Outflow of Fluid

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Topics: Cavities , Fluids , Heat transfer , Outflow , Disks , Flow (Dynamics) , Flow visualization , Ekman dynamics , Momentum

New Heat Transfer Gages for Use on Multilayered Substrates

J. E. Doorly, M. L. G. Oldfield

J. Turbomach. July 1986, 108(1): 153–160. doi: https://doi.org/10.1115/1.3262015

Abstract

View articletitled, New Heat Transfer Gages for Use on Multilayered Substrates

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Topics: Gages , Heat transfer , Calibration , Durability , Enameling , Flow (Dynamics) , Instrumentation , Metals , Thin films , Turbines

Discussions

Discussion: “The Development of a Second Generation of Controlled Diffusion Airfoils for Multistage Compressors” (Behlke, R. F., 1986, ASME J. Turbomach., 108, pp. 32–40)

I. G. Rice, P.E.

J. Turbomach. July 1986, 108(1): 40–41. doi: https://doi.org/10.1115/1.3262021

View articletitled, Discussion: “The Development of a Second Generation of Controlled Diffusion Airfoils for Multistage Compressors” (Behlke, R. F., 1986, ASME J. Turbomach., 108, pp. 32–40)

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Topics: Airfoils , Compressors , Diffusion (Physics)

Closure to “Discussion of ‘The Development of a Second Generation of Controlled Diffusion Airfoils for Multistage Compressors’” (1986, ASME J. Turbomach., 108, pp. 40–41)

R. F. Behlke

J. Turbomach. July 1986, 108(1): 41. doi: https://doi.org/10.1115/1.3262022

View articletitled, Closure to “Discussion of ‘The Development of a Second Generation of Controlled Diffusion Airfoils for Multistage Compressors’” (1986, ASME J. Turbomach., 108, pp. 40–41)

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Topics: Airfoils , Diffusion (Physics)

Editorial

Editorial

Research Papers

Spanwise Mixing in Multistage Axial Flow Compressors: Part I—Experimental Investigation

Spanwise Mixing in Multistage Axial Flow Compressors: Part II—Throughflow Calculations Including Mixing

Through-Flow Analysis of a Multistage Compressor: Part I—Aerodynamic Input

Through-Flow Analysis of a Multistage Compressor: Part II—Analytical-Experimental Comparisons

The Development of a Second Generation of Controlled Diffusion Airfoils for Multistage Compressors

Comparison of Calculated and Experimental Cascade Performance for Controlled-Diffusion Compressor Stator Blading

Study of Three-Dimensional Viscous Flows in an Axial Compressor Cascade Including Tip Leakage Effects Using a SIMPLE-Based Algorithm

On the Application of a Linearized Unsteady Potential-Flow Analysis to Fan-Tip Cascades

Computation of Inviscid Incompressible Flow Using the Primitive Variable Formulation

Performance of Axial Compressor With Nonuniform Exit Static Pressure

Predictive Surge Control and Optimization for a Centrifugal Compressor

Heat-Flux Measurements for the Rotor of a Full-Stage Turbine: Part I—Time-Averaged Results

Heat-Flux Measurements for the Rotor of a Full-Stage Turbine: Part II—Description of Analysis Technique and Typical Time-Resolved Measurements

Heat-Flux and Pressure Measurements and Comparison With Prediction for a Low-Aspect-Ratio Turbine Stage

Laminar and Transitional Boundary Layer Structures in Accelerating Flow With Heat Transfer

Systematic Study of Film Cooling With a Three-Dimensional Calculation Procedure

Heat Transfer Downstream of a Leading Edge Separation Bubble

Flat-Plate Film Cooling With Steam Injection Through One Row and Two Rows of Inclined Holes

The Effect of Inlet Conditions on Heat Transfer in a Rotating Cavity With a Radial Outflow of Fluid

New Heat Transfer Gages for Use on Multilayered Substrates

Discussions

Discussion: “The Development of a Second Generation of Controlled Diffusion Airfoils for Multistage Compressors” (Behlke, R. F., 1986, ASME J. Turbomach., 108, pp. 32–40)

Closure to “Discussion of ‘The Development of a Second Generation of Controlled Diffusion Airfoils for Multistage Compressors’” (1986, ASME J. Turbomach., 108, pp. 40–41)

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