Volume 117 Issue 1 | J. Turbomach. | ASME Digital Collection

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Volume 117, Issue 1

January 1995

ISSN 0889-504X

EISSN 1528-8900

Research Papers

Darryl E. Metzger Memorial Session Paper: A Summary of the Cooled Turbine Blade Tip Heat Transfer and Film Effectiveness Investigations Performed by Dr. D. E. Metzger

Y. W. Kim, J. P. Downs, F. O. Soechting, W. Abdel-Messeh, G. D. Steuber, S. Tanrikut

J. Turbomach. January 1995, 117(1): 1–11. doi: https://doi.org/10.1115/1.2835638

Abstract

View articletitled, <em>Darryl E. Metzger Memorial Session Paper</em>: A Summary of the Cooled Turbine Blade Tip Heat Transfer and Film Effectiveness Investigations Performed by Dr. D. E. Metzger

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Topics: Heat transfer , Turbine blades , Blades , Clearances (Engineering) , Coolants , Pressure , Flow (Dynamics) , Airfoils , Film cooling , Leakage flows

Heat Transfer and Effectiveness on Film Cooled Turbine Blade Tip Models

Y. W. Kim, D. E. Metzger

J. Turbomach. January 1995, 117(1): 12–21. doi: https://doi.org/10.1115/1.2835630

Abstract

View articletitled, Heat Transfer and Effectiveness on Film Cooled Turbine Blade Tip Models

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Topics: Heat transfer , Turbine blades , Blades , Clearances (Engineering) , Pressure , Flow (Dynamics) , Convection , Leakage flows , Coolants , Film flow

Three-Dimensional Flow in a Highly Loaded Single-Stage Transonic Fan

J. D. Bryce, M. A. Cherrett, P. A. Lyes

J. Turbomach. January 1995, 117(1): 22–28. doi: https://doi.org/10.1115/1.2835640

Abstract

View articletitled, Three-Dimensional Flow in a Highly Loaded Single-Stage Transonic Fan

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Topics: Flow (Dynamics) , Stators , Instrumentation , Blades , Corners (Structural elements) , Design , Flow measurement , Flow visualization , Rotors

Measurements of the Flow Field Within a Compressor Outlet Guide Vane Passage

J. F. Carrotte, K. F. Young, S. J. Stevens

J. Turbomach. January 1995, 117(1): 29–37. doi: https://doi.org/10.1115/1.2835641

Abstract

View articletitled, Measurements of the Flow Field Within a Compressor Outlet Guide Vane Passage

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Topics: Compressors , Flow (Dynamics) , Guide vanes , Blades , Pressure , Rotors , Vorticity , Annulus , Chords (Trusses) , Design

Turbulence Intensity and Length Scale Measurements in Multistage Compressors

T. R. Camp, H.-W. Shin

J. Turbomach. January 1995, 117(1): 38–46. doi: https://doi.org/10.1115/1.2835642

Abstract

View articletitled, Turbulence Intensity and Length Scale Measurements in Multistage Compressors

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Topics: Compressors , Turbulence , Design , Flow (Dynamics) , Turbomachinery , Blades , Computational fluid dynamics , Modeling

Control-Oriented High-Frequency Turbomachinery Modeling: Single-Stage Compression System One-Dimensional Model

O. O. Badmus, S. Chowdhury, K. M. Eveker, C. N. Nett

J. Turbomach. January 1995, 117(1): 47–61. doi: https://doi.org/10.1115/1.2835643

Abstract

View articletitled, Control-Oriented High-Frequency Turbomachinery Modeling: Single-Stage Compression System One-Dimensional Model

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Topics: Compression , Modeling , Turbomachinery , Compressors , Control equipment , Nozzles , Surges , Bifurcation , Design , Entropy

Prestall Behavior of Several High-Speed Compressors

M. Tryfonidis, O. Etchevers, J. D. Paduano, A. H. Epstein, G. J. Hendricks

J. Turbomach. January 1995, 117(1): 62–80. doi: https://doi.org/10.1115/1.2835644

Abstract

View articletitled, Prestall Behavior of Several High-Speed Compressors

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Topics: Compressors , Waves , Stability , Machinery , Rotors , Stall inception , Traveling waves , Compressibility , Design , Dynamics (Mechanics)

Monitoring of Aerodynamic Load and Detection of Stall in Multistage Axial Compressors

H. Ho¨nen, H. E. Gallus

J. Turbomach. January 1995, 117(1): 81–86. doi: https://doi.org/10.1115/1.2835645

Abstract

View articletitled, Monitoring of Aerodynamic Load and Detection of Stall in Multistage Axial Compressors

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Topics: Compressors , Stress , Axial flow , Fluctuations (Physics) , Gas turbines , High pressure (Physics) , Monitoring systems , Probes , Signals , Spectra (Spectroscopy)

Rotating Stall Acoustic Signature in a Low-Speed Centrifugal Compressor: Part 1—Vaneless Diffuser

P. B. Lawless, S. Fleeter

J. Turbomach. January 1995, 117(1): 87–96. doi: https://doi.org/10.1115/1.2835646

Abstract

View articletitled, Rotating Stall Acoustic Signature in a Low-Speed Centrifugal Compressor: Part 1—Vaneless Diffuser

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Topics: Acoustics , Compressors , Vaneless diffusers , Pressure , Waves , Fourier analysis , Impellers , Microphones , Diffusers , Excitation

Control of the Unsteady Flow in a Stator Blade Row Interacting With Upstream Moving Wakes

T. Valkov, C. S. Tan

J. Turbomach. January 1995, 117(1): 97–105. doi: https://doi.org/10.1115/1.2835647

Abstract

View articletitled, Control of the Unsteady Flow in a Stator Blade Row Interacting With Upstream Moving Wakes

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Topics: Blades , Stators , Unsteady flow , Wakes , Pressure , Suction , Vortices , Boundary layers , Fluctuations (Physics) , Fluids

Experimental and Numerical Study of the Time-Dependent Pressure Response of a Shock Wave Oscillating in a Nozzle

P. Ott, A. Bo¨lcs, T. H. Fransson

J. Turbomach. January 1995, 117(1): 106–114. doi: https://doi.org/10.1115/1.2835625

Abstract

View articletitled, Experimental and Numerical Study of the Time-Dependent Pressure Response of a Shock Wave Oscillating in a Nozzle

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Topics: Nozzles , Pressure , Shock waves , Shock (Mechanics) , Pressure transducers , Excitation , Blades , Boundary layers , Flow (Dynamics) , Flow visualization

Leading Edge Separation Bubbles on Turbomachine Blades

R. E. Walraevens, N. A. Cumpsty

J. Turbomach. January 1995, 117(1): 115–125. doi: https://doi.org/10.1115/1.2835626

Abstract

View articletitled, Leading Edge Separation Bubbles on Turbomachine Blades

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Topics: Blades , Bubbles , Separation (Technology) , Turbomachinery , Turbulence , Airfoils , Boundary layers , Compressors , Reynolds number , Shapes

Investigation of Throughflow Hypothesis in a Turbine Cascade Using a Three-Dimensional Navier–Stokes Computation

G. Perrin, F. Leboeuf

J. Turbomach. January 1995, 117(1): 126–132. doi: https://doi.org/10.1115/1.2835629

Abstract

View articletitled, Investigation of Throughflow Hypothesis in a Turbine Cascade Using a Three-Dimensional Navier–Stokes Computation

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Topics: Cascades (Fluid dynamics) , Computation , Turbines , Blades , Fluctuations (Physics) , Kinetic energy , Momentum , Convection , Energy dissipation , Flow (Dynamics)

The Influence of Load Distribution on Secondary Flow in Straight Turbine Cascades

A. P. Weiss, L. Fottner

J. Turbomach. January 1995, 117(1): 133–141. doi: https://doi.org/10.1115/1.2835631

Abstract

View articletitled, The Influence of Load Distribution on Secondary Flow in Straight Turbine Cascades

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Topics: Flow (Dynamics) , Stress , Turbines , Cascades (Fluid dynamics) , Flow visualization , Pressure , Probes

Osborne Reynolds: Energy Methods in Transition and Loss Production: A Centennial Perspective

J. Moore, J. G. Moore

J. Turbomach. January 1995, 117(1): 142–153. doi: https://doi.org/10.1115/1.2835632

Abstract

View articletitled, Osborne Reynolds: Energy Methods in Transition and Loss Production: A Centennial Perspective

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Topics: Boundary layers , Channel flow , Energy budget (Physics) , Flow (Dynamics) , Kinetic energy , Modeling , Pipes , Reynolds number , Stress , Turbulence

Effects of Criterion Functions on Intermittency in Heated Transitional Boundary Layers With and Without Streamwise Acceleration

F. J. Keller, T. Wang

J. Turbomach. January 1995, 117(1): 154–165. doi: https://doi.org/10.1115/1.2835633

Abstract

View articletitled, Effects of Criterion Functions on Intermittency in Heated Transitional Boundary Layers With and Without Streamwise Acceleration

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Topics: Boundary layers , Turbulence , Flow (Dynamics) , Pressure gradient , Momentum , Shear stress , Temperature

Bypass Transition in Boundary Layers Including Curvature and Favorable Pressure Gradient Effects

R. J. Volino, T. W. Simon

J. Turbomach. January 1995, 117(1): 166–174. doi: https://doi.org/10.1115/1.2835634

Abstract

View articletitled, Bypass Transition in Boundary Layers Including Curvature and Favorable Pressure Gradient Effects

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Topics: Boundary layers , Pressure gradient , Turbulence , Skin friction (Fluid dynamics) , Flow (Dynamics) , Momentum , Reynolds number , Enthalpy , Vortices

Experimental and Theoretical Investigations of Heat Transfer in Closed Gas-Filled Rotating Annuli

D. Bohn, E. Deuker, R. Emunds, V. Gorzelitz

J. Turbomach. January 1995, 117(1): 175–183. doi: https://doi.org/10.1115/1.2835635

Abstract

View articletitled, Experimental and Theoretical Investigations of Heat Transfer in Closed Gas-Filled Rotating Annuli

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Topics: Annulus , Heat transfer , Cavities , Heat flux , Flow (Dynamics) , Rotors , Centrifugal force , Computer software , Convection , Density

An Advanced Method of Processing Liquid Crystal Video Signals From Transient Heat Transfer Experiments

Z. Wang, P. T. Ireland, T. V. Jones

J. Turbomach. January 1995, 117(1): 184–189. doi: https://doi.org/10.1115/1.2835636

Abstract

View articletitled, An Advanced Method of Processing Liquid Crystal Video Signals From Transient Heat Transfer Experiments

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Topics: Liquid crystals , Signals , Transient heat transfer , Cooling , Film cooling , Heat transfer coefficients , Turbine blades

A Numerical Simulation of a Brush Seal Section and Some Experimental Results

M. J. Braun, V. V. Kudriavtsev

J. Turbomach. January 1995, 117(1): 190–202. doi: https://doi.org/10.1115/1.2835637

Abstract

View articletitled, A Numerical Simulation of a Brush Seal Section and Some Experimental Results

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Topics: Computer simulation , Flow (Dynamics) , Pressure , Algorithms , Construction , Engines , Failure , Inertia (Mechanics) , Navier-Stokes equations , Performance characterization

Discussions

Discussion: “Leading Edge Separation Bubbles on Turbomachine Blades” (Walraevens, R. E., and Cumpsty, N. A., 1995, ASME J. Turbomach., 117, pp. 115–125)

L. H. Smith, Jr.

J. Turbomach. January 1995, 117(1): 125. doi: https://doi.org/10.1115/1.2835627

View articletitled, Discussion: “Leading Edge Separation Bubbles on Turbomachine Blades” (Walraevens, R. E., and Cumpsty, N. A., 1995, ASME J. Turbomach., 117, pp. 115–125)

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Topics: Blades , Bubbles , Separation (Technology) , Turbomachinery

Closure to “Discussion of ‘Leading Edge Separation Bubbles on Turbomachine Blades’” (1995, ASME J. Turbomach., 117, p. 125)

R. E. Walraevens, N. A. Cumpsty

J. Turbomach. January 1995, 117(1): 125. doi: https://doi.org/10.1115/1.2835628

View articletitled, Closure to “Discussion of ‘Leading Edge Separation Bubbles on Turbomachine Blades’” (1995, ASME J. Turbomach., 117, p. 125)

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Topics: Bubbles , Separation (Technology) , Turbomachinery

Technical Briefs

A Note on Turbine Cooling Performance Characterization

D. A. Nealy

J. Turbomach. January 1995, 117(1): 203–204. doi: https://doi.org/10.1115/1.2835639

View articletitled, A Note on Turbine Cooling Performance Characterization

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Topics: Cooling , Performance characterization , Turbines

Research Papers

Darryl E. Metzger Memorial Session Paper: A Summary of the Cooled Turbine Blade Tip Heat Transfer and Film Effectiveness Investigations Performed by Dr. D. E. Metzger

Heat Transfer and Effectiveness on Film Cooled Turbine Blade Tip Models

Three-Dimensional Flow in a Highly Loaded Single-Stage Transonic Fan

Measurements of the Flow Field Within a Compressor Outlet Guide Vane Passage

Turbulence Intensity and Length Scale Measurements in Multistage Compressors

Control-Oriented High-Frequency Turbomachinery Modeling: Single-Stage Compression System One-Dimensional Model

Prestall Behavior of Several High-Speed Compressors

Monitoring of Aerodynamic Load and Detection of Stall in Multistage Axial Compressors

Rotating Stall Acoustic Signature in a Low-Speed Centrifugal Compressor: Part 1—Vaneless Diffuser

Control of the Unsteady Flow in a Stator Blade Row Interacting With Upstream Moving Wakes

Experimental and Numerical Study of the Time-Dependent Pressure Response of a Shock Wave Oscillating in a Nozzle

Leading Edge Separation Bubbles on Turbomachine Blades

Investigation of Throughflow Hypothesis in a Turbine Cascade Using a Three-Dimensional Navier–Stokes Computation

The Influence of Load Distribution on Secondary Flow in Straight Turbine Cascades

Osborne Reynolds: Energy Methods in Transition and Loss Production: A Centennial Perspective

Effects of Criterion Functions on Intermittency in Heated Transitional Boundary Layers With and Without Streamwise Acceleration

Bypass Transition in Boundary Layers Including Curvature and Favorable Pressure Gradient Effects

Experimental and Theoretical Investigations of Heat Transfer in Closed Gas-Filled Rotating Annuli

An Advanced Method of Processing Liquid Crystal Video Signals From Transient Heat Transfer Experiments

A Numerical Simulation of a Brush Seal Section and Some Experimental Results

Discussions

Discussion: “Leading Edge Separation Bubbles on Turbomachine Blades” (Walraevens, R. E., and Cumpsty, N. A., 1995, ASME J. Turbomach., 117, pp. 115–125)

Closure to “Discussion of ‘Leading Edge Separation Bubbles on Turbomachine Blades’” (1995, ASME J. Turbomach., 117, p. 125)

Technical Briefs

A Note on Turbine Cooling Performance Characterization

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