Volume 126 Issue 1 | J. Turbomach. | ASME Digital Collection

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Technical Papers

Backward Traveling Rotating Stall Waves in Centrifugal Compressors

Z. S. Spakovszky

J. Turbomach. January 2004, 126(1): 1–12. doi: https://doi.org/10.1115/1.1643382

Abstract

View articletitled, Backward Traveling Rotating Stall Waves in Centrifugal Compressors

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Topics: Compressors , Design , Diffusers , Flow (Dynamics) , Impellers , Rotors , Stability , Surges , Waves , Blades

The Effects of Wake-Passing Unsteadiness Over a Highly Loaded Compressor-Like Flat Plate

Xavier Ottavy, Stephane Vilmin, Howard Hodson, Simon Gallimore

J. Turbomach. January 2004, 126(1): 13–23. doi: https://doi.org/10.1115/1.1643384

Abstract

View articletitled, The Effects of Wake-Passing Unsteadiness Over a Highly Loaded Compressor-Like Flat Plate

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Topics: Boundary layers , Computational fluid dynamics , Flow (Dynamics) , Shapes , Turbulence , Wakes , Compressors , Separation (Technology) , Flat plates , Bubbles

Active Flow Separation Control of a Stator Vane Using Embedded Injection in a Multistage Compressor Experiment

Dennis E. Culley, Michelle M. Bright, Patricia S. Prahst, Anthony J. Strazisar

J. Turbomach. January 2004, 126(1): 24–34. doi: https://doi.org/10.1115/1.1643912

Abstract

View articletitled, Active Flow Separation Control of a Stator Vane Using Embedded Injection in a Multistage Compressor Experiment

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Topics: Compressors , Flow (Dynamics) , Flow control , Pressure , Separation (Technology) , Stators , Valves , Suction , Design , Momentum

Aerodynamic Blade Row Interactions in an Axial Compressor—Part I: Unsteady Boundary Layer Development

Ronald Mailach, Konrad Vogeler

J. Turbomach. January 2004, 126(1): 35–44. doi: https://doi.org/10.1115/1.1649741

Abstract

View articletitled, Aerodynamic Blade Row Interactions in an Axial Compressor—Part I: Unsteady Boundary Layer Development

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Topics: Blades , Boundary layers , Compressors , Flow (Dynamics) , Turbulence , Wakes , Design , Stators , Suction , Rotors

Aerodynamic Blade Row Interactions in an Axial Compressor—Part II: Unsteady Profile Pressure Distribution and Blade Forces

Ronald Mailach, Konrad Vogeler

J. Turbomach. January 2004, 126(1): 45–51. doi: https://doi.org/10.1115/1.1649742

Abstract

View articletitled, Aerodynamic Blade Row Interactions in an Axial Compressor—Part II: Unsteady Profile Pressure Distribution and Blade Forces

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Topics: Blades , Pressure , Stators , Wakes , Design , Rotors , Compressors

Tailored Structural Design and Aeromechanical Control of Axial Compressor Stall—Part I: Development of Models and Metrics

O. G. McGee, M. B. Graf, L. G. Fre´chette

J. Turbomach. January 2004, 126(1): 52–62. doi: https://doi.org/10.1115/1.1644555

Abstract

View articletitled, Tailored Structural Design and Aeromechanical Control of Axial Compressor Stall—Part I: Development of Models and Metrics

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Topics: Compression , Compressors , Control equipment , Feedback , Flow (Dynamics) , Pressure , Stability , Dynamics (Mechanics) , Modeling , Damping

Tailored Structural Design and Aeromechanical Control of Axial Compressor Stall—Part II: Evaluation of Approaches

L. G. Fre´chette, O. G. McGee, M. B. Graf

J. Turbomach. January 2004, 126(1): 63–72. doi: https://doi.org/10.1115/1.1644556

Abstract

View articletitled, Tailored Structural Design and Aeromechanical Control of Axial Compressor Stall—Part II: Evaluation of Approaches

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Topics: Compressors , Damping , Feedback , Flow (Dynamics) , Dynamics (Mechanics) , Pressure , Fluids , Control equipment , Blades

Investigation of an Inversely Designed Centrifugal Compressor Stage—Part I: Design and Numerical Verification

M. Zangeneh, M. Schleer, F. Pløger, S. S. Hong, C. Roduner, B. Ribi, R. S. Abhari

J. Turbomach. January 2004, 126(1): 73–81. doi: https://doi.org/10.1115/1.1645868

Abstract

View articletitled, Investigation of an Inversely Designed Centrifugal Compressor Stage—Part I: Design and Numerical Verification

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Topics: Blades , Computational fluid dynamics , Design , Geometry , Impellers , Flow (Dynamics) , Compressors , Computation , Pressure

Investigation of an Inversely Designed Centrifugal Compressor Stage—Part II: Experimental Investigations

M. Schleer, S. S. Hong, M. Zangeneh, C. Roduner, B. Ribi, F. Pløger, R. S. Abhari

J. Turbomach. January 2004, 126(1): 82–90. doi: https://doi.org/10.1115/1.1625690

Abstract

View articletitled, Investigation of an Inversely Designed Centrifugal Compressor Stage—Part II: Experimental Investigations

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Topics: Compressors , Design , Flow (Dynamics) , Impellers , Pressure , Diffusers , Blades

Numerical Optimization of Turbomachinery Bladings

Ste´phane Burguburu, Clement Toussaint, Christophe Bonhomme, Gilles Leroy

J. Turbomach. January 2004, 126(1): 91–100. doi: https://doi.org/10.1115/1.1645869

Abstract

View articletitled, Numerical Optimization of Turbomachinery Bladings

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Topics: Optimization , Design , Blades , Flow (Dynamics) , Deformation

Heat-Transfer Measurements and Predictions for the Vane and Blade of a Rotating High-Pressure Turbine Stage

Charles W. Haldeman, Michael G. Dunn

J. Turbomach. January 2004, 126(1): 101–109. doi: https://doi.org/10.1115/1.1626132

Abstract

View articletitled, Heat-Transfer Measurements and Predictions for the Vane and Blade of a Rotating High-Pressure Turbine Stage

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Topics: Blades , Heat transfer , Reynolds number , Turbines , Pressure , Instrumentation , Heat flux , High pressure (Physics) , Boundary layers

Measurements and Predictions of Heat Transfer on Rotor Blades in a Transonic Turbine Cascade

Paul W. Giel, Robert J. Boyle, Ronald S. Bunker

J. Turbomach. January 2004, 126(1): 110–121. doi: https://doi.org/10.1115/1.1643383

Abstract

View articletitled, Measurements and Predictions of Heat Transfer on Rotor Blades in a Transonic Turbine Cascade

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Topics: Blades , Heat transfer , Pressure , Reynolds number , Turbulence , Flow (Dynamics) , Cascades (Fluid dynamics)

Flow Field Computations of Combustor-Turbine Interactions Relevant to a Gas Turbine Engine

Sarah Stitzel, Karen A. Thole

J. Turbomach. January 2004, 126(1): 122–129. doi: https://doi.org/10.1115/1.1625691

Abstract

View articletitled, Flow Field Computations of Combustor-Turbine Interactions Relevant to a Gas Turbine Engine

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Topics: Combustion chambers , Flow (Dynamics) , Pressure , Turbines , Film cooling , Gas turbines

Effect of Blade Tip Geometry on Tip Flow and Heat Transfer for a Blade in a Low-Speed Cascade

Vikrant Saxena, Hasan Nasir, Srinath V. Ekkad, Assistant Professor, Mem. ASME

J. Turbomach. January 2004, 126(1): 130–138. doi: https://doi.org/10.1115/1.1643385

Abstract

View articletitled, Effect of Blade Tip Geometry on Tip Flow and Heat Transfer for a Blade in a Low-Speed Cascade

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Topics: Blades , Cascades (Fluid dynamics) , Flow (Dynamics) , Heat transfer , Heat transfer coefficients , Leakage flows , Wakes , Liquid crystals , Strips , Turbulence

Measurement and Prediction of Heat Transfer Distributions on an Aft-Loaded Vane Subjected to the Influence of Catalytic and Dry Low ${NO}_{x}$ Combustor Turbulence

F. E. Ames, M. Argenziano, C. Wang

J. Turbomach. January 2004, 126(1): 139–149. doi: https://doi.org/10.1115/1.1645867

Abstract

View articletitled, Measurement and Prediction of Heat Transfer Distributions on an Aft-Loaded Vane Subjected to the Influence of Catalytic and Dry Low <span class="inline-formula no-formula-id"><span class="mathFormula"></span><math xmlns="http://www.w3.org/1998/Math/MathML"><mrow xmlns=""><msub><mtext mathvariant="italic">NO</mtext><mrow><mi>x</mi></mrow></msub></mrow></math></span> Combustor Turbulence

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Topics: Combustion chambers , Heat transfer , Turbulence , Pressure , Reynolds number , Nitrogen oxides

Mistuning Identification of Bladed Disks Using a Fundamental Mistuning Model—Part I: Theory

D. M. Feiner, J. H. Griffin

J. Turbomach. January 2004, 126(1): 150–158. doi: https://doi.org/10.1115/1.1643913

Abstract

View articletitled, Mistuning Identification of Bladed Disks Using a Fundamental Mistuning Model—Part I: Theory

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Topics: Blades , Disks , Rotors , Finite element model

Mistuning Identification of Bladed Disks Using a Fundamental Mistuning Model—Part II: Application

D. M. Feiner, J. H. Griffin

J. Turbomach. January 2004, 126(1): 159–165. doi: https://doi.org/10.1115/1.1643914

Abstract

View articletitled, Mistuning Identification of Bladed Disks Using a Fundamental Mistuning Model—Part II: Application

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Topics: Blades , Disks , Rotors , Compressors , Torsion

Experimental and Numerical Study of Stall Flutter in a Transonic Low-Aspect Ratio Fan Blisk

A. J. Sanders, K. K. Hassan, D. C. Rabe

J. Turbomach. January 2004, 126(1): 166–174. doi: https://doi.org/10.1115/1.1645532

Abstract

View articletitled, Experimental and Numerical Study of Stall Flutter in a Transonic Low-Aspect Ratio Fan Blisk

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Topics: Computational fluid dynamics , Flutter (Aerodynamics) , Pressure , Clearances (Engineering) , Simulation , Flow (Dynamics) , Cycles

A Method for Use of Cyclic Symmetry Properties in Analysis of Nonlinear Multiharmonic Vibrations of Bladed Disks

E. P. Petrov

J. Turbomach. January 2004, 126(1): 175–183. doi: https://doi.org/10.1115/1.1644558

Abstract

View articletitled, A Method for Use of Cyclic Symmetry Properties in Analysis of Nonlinear Multiharmonic Vibrations of Bladed Disks

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Topics: Disks , Excitation , Vibration , Nonlinear equations

Generic Friction Models for Time-Domain Vibration Analysis of Bladed Disks

E. P. Petrov, D. J. Ewins

J. Turbomach. January 2004, 126(1): 184–192. doi: https://doi.org/10.1115/1.1644557

Abstract

View articletitled, Generic Friction Models for Time-Domain Vibration Analysis of Bladed Disks

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Topics: Friction , Stress

A New Model for Boundary Layer Transition Using a Single-Point RANS Approach

D. Keith Walters, James H. Leylek

J. Turbomach. January 2004, 126(1): 193–202. doi: https://doi.org/10.1115/1.1622709

Abstract

View articletitled, A New Model for Boundary Layer Transition Using a Single-Point RANS Approach

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Topics: Boundary layers , Turbulence , Fluctuations (Physics) , Flow (Dynamics) , Viscosity

The Effects of High Mainstream Turbulence and Turbine Vane Film Cooling on the Dispersion of a Simulated Hot Streak

Sean Jenkins, Krishnakumar Varadarajan, David G. Bogard

J. Turbomach. January 2004, 126(1): 203–211. doi: https://doi.org/10.1115/1.1643911

Abstract

View articletitled, The Effects of High Mainstream Turbulence and Turbine Vane Film Cooling on the Dispersion of a Simulated Hot Streak

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Topics: Film cooling , Pressure , Suction , Temperature , Turbulence , Coolants , Turbines , Flow (Dynamics)

Pressure and Flow Characteristics in a Rotating Two-Pass Square Duct With 45-Deg Angled Ribs

Tong-Miin Liou, Professor and Dean, Fellow ASME, Guang-Yuan Dai, Graduate Student

J. Turbomach. January 2004, 126(1): 212–219. doi: https://doi.org/10.1115/1.1649744

Abstract

View articletitled, Pressure and Flow Characteristics in a Rotating Two-Pass Square Duct With 45-Deg Angled Ribs

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Topics: Ducts , Flow (Dynamics) , Pressure , Rotation , Vortices , Friction , Turbulence , Fluid dynamics , Computational fluid dynamics

Technical Papers

Backward Traveling Rotating Stall Waves in Centrifugal Compressors

The Effects of Wake-Passing Unsteadiness Over a Highly Loaded Compressor-Like Flat Plate

Active Flow Separation Control of a Stator Vane Using Embedded Injection in a Multistage Compressor Experiment

Aerodynamic Blade Row Interactions in an Axial Compressor—Part I: Unsteady Boundary Layer Development

Aerodynamic Blade Row Interactions in an Axial Compressor—Part II: Unsteady Profile Pressure Distribution and Blade Forces

Tailored Structural Design and Aeromechanical Control of Axial Compressor Stall—Part I: Development of Models and Metrics

Tailored Structural Design and Aeromechanical Control of Axial Compressor Stall—Part II: Evaluation of Approaches

Investigation of an Inversely Designed Centrifugal Compressor Stage—Part I: Design and Numerical Verification

Investigation of an Inversely Designed Centrifugal Compressor Stage—Part II: Experimental Investigations

Numerical Optimization of Turbomachinery Bladings

Heat-Transfer Measurements and Predictions for the Vane and Blade of a Rotating High-Pressure Turbine Stage

Measurements and Predictions of Heat Transfer on Rotor Blades in a Transonic Turbine Cascade

Flow Field Computations of Combustor-Turbine Interactions Relevant to a Gas Turbine Engine

Effect of Blade Tip Geometry on Tip Flow and Heat Transfer for a Blade in a Low-Speed Cascade

Measurement and Prediction of Heat Transfer Distributions on an Aft-Loaded Vane Subjected to the Influence of Catalytic and Dry Low ${NO}_{x}$ Combustor Turbulence

Mistuning Identification of Bladed Disks Using a Fundamental Mistuning Model—Part I: Theory

Mistuning Identification of Bladed Disks Using a Fundamental Mistuning Model—Part II: Application

Experimental and Numerical Study of Stall Flutter in a Transonic Low-Aspect Ratio Fan Blisk

A Method for Use of Cyclic Symmetry Properties in Analysis of Nonlinear Multiharmonic Vibrations of Bladed Disks

Generic Friction Models for Time-Domain Vibration Analysis of Bladed Disks

A New Model for Boundary Layer Transition Using a Single-Point RANS Approach

The Effects of High Mainstream Turbulence and Turbine Vane Film Cooling on the Dispersion of a Simulated Hot Streak

Pressure and Flow Characteristics in a Rotating Two-Pass Square Duct With 45-Deg Angled Ribs

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