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Proceedings Papers

Observations of Separated Laminar Flow on Axial Compressor Blading

G. J. Walker

Proc. ASME. GT1975, Volume 1B: General, V01BT02A001, March 2–6, 1975

Paper No: 75-GT-63

DOI: https://doi.org/10.1115/75-GT-63

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Topics: Compressors, Laminar flow, Bubbles, Separation (Technology), Blades, Reynolds number

Proceedings Papers

The Turbulent Boundary Layer on an Axial Compressor Blade

G. J. Walker

Proc. ASME. GT1982, Volume 1: Turbomachinery, V001T01A022, April 18–22, 1982

Paper No: 82-GT-52

DOI: https://doi.org/10.1115/82-GT-52

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Topics: Blades, Boundary layer turbulence, Compressors, Reynolds number, Boundary layers, Boundary-value problems, Chords (Trusses), Computational methods, Equilibrium (Physics), Errors

Proceedings Papers

Transition Modeling Effects on Viscous/Inviscid Interaction Analysis of Low Reynolds Number Airfoil Flows Involving Laminar Separation Bubbles

G. J. Walker, P. H. Subroto, M. F. Platzer

Proc. ASME. GT1988, Volume 1: Turbomachinery, V001T01A007, June 6–9, 1988

Paper No: 88-GT-32

DOI: https://doi.org/10.1115/88-GT-32

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Topics: Airfoils, Bubbles, Flow (Dynamics), Modeling, Reynolds number, Separation (Technology), Blades, Chords (Trusses), Pressure gradient, Turbulence

Proceedings Papers

Similarity Behavior in Transitional Boundary Layers Over a Range of Adverse Pressure Gradients and Turbulence Levels

J. P. Gostelow, G. J. Walker

Proc. ASME. GT1990, Volume 1: Turbomachinery, V001T01A037, June 11–14, 1990

Paper No: 90-GT-130

DOI: https://doi.org/10.1115/90-GT-130

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Topics: Boundary layers, Pressure gradient, Turbulence, Equilibrium (Physics), Boundary layer turbulence, Shear stress, Skin friction (Fluid dynamics)

Proceedings Papers

Boundary Layer and Navier-Stokes Analysis of a NASA Controlled-Diffusion Compressor Blade

Y. K. Ho, G. J. Walker, P. Stow

Proc. ASME. GT1990, Volume 1: Turbomachinery, V001T01A083, June 11–14, 1990

Paper No: 90-GT-236

DOI: https://doi.org/10.1115/90-GT-236

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Topics: Blades, Boundary layers, Compressors, Diffusion (Physics), NASA, Design, Modeling, Boundary layer turbulence, Bubbles, Computational methods

Proceedings Papers

Effects of Adverse Pressure Gradients on the Nature and Length of Boundary Layer Transition

G. J. Walker, J. P. Gostelow

Proc. ASME. GT1989, Volume 1: Turbomachinery, V001T01A096, June 4–8, 1989

Paper No: 89-GT-274

DOI: https://doi.org/10.1115/89-GT-274

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Topics: Boundary layers, Pressure gradient, Waves, Flow (Dynamics), Reynolds number, Separation (Technology), Turbulence

Proceedings Papers

Stator Averaged, Rotor Blade-to-Blade Near Wall Flow in a Multistage Axial Compressor With Tip Clearance Variation

I. N. Moyle, G. J. Walker, R. P. Shreeve

Proc. ASME. GT1991, Volume 1: Turbomachinery, V001T01A009, June 3–6, 1991

Paper No: 91-GT-030

DOI: https://doi.org/10.1115/91-GT-030

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Topics: Blades, Clearances (Engineering), Compressors, Flow (Dynamics), Rotors, Stators, Pressure, Die cutting, Shear (Mechanics), Shearing (Deformation)

Proceedings Papers

The Role of Laminar-Turbulent Transition in Gas Turbine Engines: A Discussion

G. J. Walker

Proc. ASME. GT1992, Volume 1: Turbomachinery, V001T01A108, June 1–4, 1992

Paper No: 92-GT-301

DOI: https://doi.org/10.1115/92-GT-301

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Topics: Gas turbines, Turbulence, Pressure gradient, Blades, Bubbles, Flow (Dynamics), Physics, Separation (Technology), Turbomachinery

Proceedings Papers

Effects of Free-Stream Turbulence and Adverse Pressure Gradients on Boundary Layer Transition

J. P. Gostelow, A. R. Blunden, G. J. Walker

Proc. ASME. GT1992, Volume 1: Turbomachinery, V001T01A128, June 1–4, 1992

Paper No: 92-GT-380

DOI: https://doi.org/10.1115/92-GT-380

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Topics: Boundary layers, Pressure gradient, Turbulence, Equilibrium (Physics), Laminar flow, Physics, Waves

Proceedings Papers

Turbulent Spot Development Under a Moderate Adverse Pressure Gradient

J. P. Gostelow, G. Hong, N. Melwani, G. J. Walker

Proc. ASME. GT1993, Volume 3C: General, V03CT17A038, May 24–27, 1993

Paper No: 93-GT-377

DOI: https://doi.org/10.1115/93-GT-377

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Topics: Pressure gradient, Turbulence, Wave packets, Boundary layers, Flat plates, Wind tunnels, Wire

Proceedings Papers

Observations of Wake-Induced Turbulent Spots on an Axial Compressor Blade

G. J. Walker, W. J. Solomon, J. P. Gostelow

Proc. ASME. GT1993, Volume 3C: General, V03CT17A039, May 24–27, 1993

Paper No: 93-GT-378

DOI: https://doi.org/10.1115/93-GT-378

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Topics: Blades, Compressors, Turbulence, Wakes, Flow (Dynamics), Boundary layers, Gages, Laminar flow, Pressure gradient, Rotors

Proceedings Papers

Modeling of Boundary Layer Transition in Turbulent Flows by Linear Combination Integral Method

J. P. Gostelow, G. Hong, G. J. Walker, J. Dey

Proc. ASME. GT1994, Volume 1: Turbomachinery, V001T01A120, June 13–16, 1994

Paper No: 94-GT-358

DOI: https://doi.org/10.1115/94-GT-358

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Topics: Boundary layers, Modeling, Turbulence, Flow (Dynamics), Pressure gradient, Reynolds number, Turbomachinery

Proceedings Papers

Transition Length Prediction for Flows With Rapidly Changing Pressure Gradients

W. J. Solomon, G. J. Walker, J. P. Gostelow

Proc. ASME. GT1995, Volume 1: Turbomachinery, V001T01A071, June 5–8, 1995

Paper No: 95-GT-241

DOI: https://doi.org/10.1115/95-GT-241

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Topics: Flow (Dynamics), Pressure gradient, Turbomachinery, Boundary layers, Computational methods, Turbulence, Blades, Computation, Errors, Finishes

Proceedings Papers

Observations of Wake-Induced Transition on an Axial Compressor Blade

W. J. Solomon, G. J. Walker

Proc. ASME. GT1995, Volume 1: Turbomachinery, V001T01A097, June 5–8, 1995

Paper No: 95-GT-381

DOI: https://doi.org/10.1115/95-GT-381

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Topics: Blades, Compressors, Wakes, Suction, Reynolds number, Gages, Pressure, Airfoils, Chords (Trusses), Design

Proceedings Papers

Effects of Streamwise Pressure Gradient on Turbulent Spot Development

J. P. Gostelow, N. Melwani, G. J. Walker

Proc. ASME. GT1995, Volume 1: Turbomachinery, V001T01A087, June 5–8, 1995

Paper No: 95-GT-303

DOI: https://doi.org/10.1115/95-GT-303

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Topics: Pressure gradient, Turbulence, Wave packets, Pressure, Blades, Boundary layer turbulence, Boundary layers, Compressors, Computer simulation, Diffusion (Physics)

Proceedings Papers

Investigation of the Calmed Region Behind a Turbulent Spot

J. P. Gostelow, G. J. Walker, W. J. Solomon, G. Hong, N. Melwani

Proc. ASME. GT1996, Volume 1: Turbomachinery, V001T01A123, June 10–13, 1996

Paper No: 96-GT-489

DOI: https://doi.org/10.1115/96-GT-489

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Topics: Turbulence, Pressure gradient, Boundary layers, Axial flow, Blades, Diffusion (Physics), Flow (Dynamics), Modeling, Rotors, Stators

Proceedings Papers

The Influence of Wake-Wake Interactions on Loss Fluctuations of a Downstream Axial Compressor Blade Row

G. J. Walker, J. D. Hughes, I. Köhler, W. J. Solomon

Proc. ASME. GT1997, Volume 1: Aircraft Engine; Marine; Turbomachinery; Microturbines and Small Turbomachinery, V001T03A085, June 2–5, 1997

Paper No: 97-GT-469

DOI: https://doi.org/10.1115/97-GT-469

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Topics: Blades, Compressors, Fluctuations (Physics), Wakes, Stators, Inlet guide vanes, Rotors, Turbomachinery, Unsteady flow, Wire

Proceedings Papers

Periodic Transition on an Axial Compressor Stator — Incidence and Clocking Effects: Part I — Experimental Data

G. J. Walker, J. D. Hughes, W. J. Solomon

Proc. ASME. GT1998, Volume 1: Turbomachinery, V001T01A090, June 2–5, 1998

Paper No: 98-GT-363

DOI: https://doi.org/10.1115/98-GT-363

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Topics: Compressors, Stators, Pressure, Flow (Dynamics), Suction, Turbulence, Wakes, Blades, Bubbles, Chords (Trusses)

Proceedings Papers

Periodic Transition on an Axial Compressor Stator — Incidence and Clocking Effects: Part II — Transition Onset Predictions

W. J. Solomon, G. J. Walker, J. D. Hughes

Proc. ASME. GT1998, Volume 1: Turbomachinery, V001T01A091, June 2–5, 1998

Paper No: 98-GT-364

DOI: https://doi.org/10.1115/98-GT-364

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Topics: Compressors, Stators, Boundary layers, Turbulence, Airfoils, Blades, Computation, Flow (Dynamics), Pressure, Separation (Technology)

Proceedings Papers

Natural Transition Phenomena on an Axial Compressor Blade

J. D. Hughes, G. J. Walker

Proc. ASME. GT2000, Volume 3: Heat Transfer; Electric Power; Industrial and Cogeneration, V003T01A069, May 8–11, 2000

Paper No: 2000-GT-0264

DOI: https://doi.org/10.1115/2000-GT-0264

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Topics: Blades, Compressors, Waves, Algorithms, Turbulence, Flow (Dynamics), Inflow, Inlet guide vanes, Probability, Stators

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Journal citation

NARROW

Observations of Separated Laminar Flow on Axial Compressor Blading

The Turbulent Boundary Layer on an Axial Compressor Blade

Transition Modeling Effects on Viscous/Inviscid Interaction Analysis of Low Reynolds Number Airfoil Flows Involving Laminar Separation Bubbles

Similarity Behavior in Transitional Boundary Layers Over a Range of Adverse Pressure Gradients and Turbulence Levels

Boundary Layer and Navier-Stokes Analysis of a NASA Controlled-Diffusion Compressor Blade

Effects of Adverse Pressure Gradients on the Nature and Length of Boundary Layer Transition

Stator Averaged, Rotor Blade-to-Blade Near Wall Flow in a Multistage Axial Compressor With Tip Clearance Variation

The Role of Laminar-Turbulent Transition in Gas Turbine Engines: A Discussion

Effects of Free-Stream Turbulence and Adverse Pressure Gradients on Boundary Layer Transition

Turbulent Spot Development Under a Moderate Adverse Pressure Gradient

Observations of Wake-Induced Turbulent Spots on an Axial Compressor Blade

Modeling of Boundary Layer Transition in Turbulent Flows by Linear Combination Integral Method

Transition Length Prediction for Flows With Rapidly Changing Pressure Gradients

Observations of Wake-Induced Transition on an Axial Compressor Blade

Effects of Streamwise Pressure Gradient on Turbulent Spot Development

Investigation of the Calmed Region Behind a Turbulent Spot

The Influence of Wake-Wake Interactions on Loss Fluctuations of a Downstream Axial Compressor Blade Row

Periodic Transition on an Axial Compressor Stator — Incidence and Clocking Effects: Part I — Experimental Data

Periodic Transition on an Axial Compressor Stator — Incidence and Clocking Effects: Part II — Transition Onset Predictions

Natural Transition Phenomena on an Axial Compressor Blade

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