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Proceedings Papers

Low-Turbulence High-Speed Wind Tunnel for the Determination of Cascade Shock Losses

J. A. Slovisky, W. B. Roberts, D. M. Sandercock

Proc. ASME. GT1979, Volume 1B: Gas Turbines, V01BT02A028, March 12–15, 1979

Publisher: American Society of Mechanical Engineers

Paper No: 79-GT-129

https://doi.org/10.1115/79-GT-129

View Paper titled, Low-Turbulence High-Speed Wind Tunnel for the Determination of Cascade Shock Losses

Topics: Cascades (Fluid dynamics), Shock (Mechanics), Turbulence, Wind tunnels, Probes, Airfoils, Chords (Trusses), Compressors, Flow (Dynamics), Flow visualization

Proceedings Papers

An Off-Design Correlation of Part Span Damper Losses Through Transonic Axial Fan Rotors

W. B. Roberts, J. E. Crouse, D. M. Sandercock

Proc. ASME. GT1979, Volume 1A: Gas Turbines, V01AT01A006, March 12–15, 1979

Publisher: American Society of Mechanical Engineers

Paper No: 79-GT-6

https://doi.org/10.1115/79-GT-6

View Paper titled, An Off-Design Correlation of Part Span Damper Losses Through Transonic Axial Fan Rotors

Topics: Dampers, Design, Rotors, Blades, Pressure, Suction

Journal Articles

Advanced Turbofan Blade Refurbishment Technique

W. B. Roberts

Publisher: ASME

J. Turbomach. October 1995, 117(4): 666–667.

https://doi.org/10.1115/1.2836586

Published Online: October 1, 1995

View Article titled, Advanced Turbofan Blade Refurbishment Technique

Topics: Blades, Turbofans

Journal Articles

The Effect of Adding Roughness and Thickness to a Transonic Axial Compressor Rotor

K. L. Suder, R. V. Chima, A. J. Strazisar, W. B. Roberts

Publisher: ASME

J. Turbomach. October 1995, 117(4): 491–505.

https://doi.org/10.1115/1.2836561

Published Online: October 1, 1995

View Article titled, The Effect of Adding Roughness and Thickness to a Transonic Axial Compressor Rotor

Topics: Compressors, Rotors, Surface roughness, Coatings, Coating processes, Blades, Design, Finishes, Airfoils, Boundary layers

Journal Articles

Discussion: “The Role of Laminar-Turbulent Transition in Gas Turbine Engines” (Mayle, Robert Edward, 1991, ASME J. Turbomach., 113, pp. 509–536)

W. B. Roberts

Publisher: ASME

J. Turbomach. October 1991, 113(4): 536–537.

https://doi.org/10.1115/1.2929111

Published Online: October 1, 1991

View Article titled, Discussion: “The Role of Laminar-Turbulent Transition in Gas Turbine Engines” (Mayle, Robert Edward, 1991, ASME J. Turbomach., 113, pp. 509–536)

Topics: Gas turbines, Turbulence

Journal Articles

Discussion: “Similarity Behavior in Transitional Boundary Layers Over a Range of Adverse Pressure Gradients and Turbulence Levels” (Gostelow, J. P., and Walker, G. J., 1991, ASME J. Turbomach., 113, pp. 617–624)

W. B. Roberts

Publisher: ASME

J. Turbomach. October 1991, 113(4): 624.

https://doi.org/10.1115/1.2929126

Published Online: October 1, 1991

View Article titled, Discussion: “Similarity Behavior in Transitional Boundary Layers Over a Range of Adverse Pressure Gradients and Turbulence Levels” (Gostelow, J. P., and Walker, G. J., 1991, ASME J. Turbomach., 113, pp. 617–624)

Topics: Boundary layers, Pressure gradient, Turbulence

Journal Articles

Design Point Variation of Three-Dimensional Loss and Deviation for Axial Compressor Middle Stages

W. B. Roberts, G. K. Serovy, D. M. Sandercock

Publisher: ASME

J. Turbomach. October 1988, 110(4): 426–433.

https://doi.org/10.1115/1.3262215

Published Online: October 1, 1988

View Article titled, Design Point Variation of Three-Dimensional Loss and Deviation for Axial Compressor Middle Stages

Topics: Compressors, Design, Blades, Boundary layers, Rotors, Clearances (Engineering), Flow (Dynamics), NASA, Pressure, Stators

Journal Articles

Discussion: “Secondary Flow, Turbulent Diffusion, and Mixing in Axial-Flow Compressors” (Wisler, D. C., Bauer, R. C., and Okiishi, T. H., 1987, ASME J. Turbomach., 109, pp. 455–469)

W. B. Roberts

Publisher: ASME

J. Turbomach. October 1987, 109(4): 477.

https://doi.org/10.1115/1.3262135

Published Online: October 1, 1987

View Article titled, Discussion: “Secondary Flow, Turbulent Diffusion, and Mixing in Axial-Flow Compressors” (Wisler, D. C., Bauer, R. C., and Okiishi, T. H., 1987, ASME J. Turbomach., 109, pp. 455–469)

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

Journal Articles

Modeling the 3-D Flow Effects on Deviation Angle for Axial Compressor Middle Stages

W. B. Roberts, G. K. Serovy, D. M. Sandercock

Publisher: ASME

J. Eng. Gas Turbines Power. January 1986, 108(1): 131–137.

https://doi.org/10.1115/1.3239859

Published Online: January 1, 1986

View Article titled, Modeling the 3-D Flow Effects on Deviation Angle for Axial Compressor Middle Stages

Topics: Compressors, Flow (Dynamics), Modeling, Blades, Boundary layers, Rotors, Stators, Approximation, Clearances (Engineering), Mach number

Journal Articles

A Design Point Correlation for Losses due to Part-Span Dampers on Transonic Rotors

W. B. Roberts

Publisher: ASME

J. Eng. Gas Turbines Power. July 1979, 101(3): 415–421.

https://doi.org/10.1115/1.3446594

Published Online: July 1, 1979

View Article titled, A Design Point Correlation for Losses due to Part-Span Dampers on Transonic Rotors

Topics: Dampers, Design, Rotors, Blades, Axial flow, Chords (Trusses), Mach number, Pressure

Journal Articles

Discussion: “A Family of Surface Velocity Distributions for Axial Compressor Blading and Their Theoretical Performance” (Walker, G. J., 1976, ASME J. Eng. Power, 98, pp. 229–238)

W. B. Roberts

Publisher: ASME

J. Eng. Gas Turbines Power. April 1976, 98(2): 239.

https://doi.org/10.1115/1.3446150

Published Online: April 1, 1976

View Article titled, Discussion: “A Family of Surface Velocity Distributions for Axial Compressor Blading and Their Theoretical Performance” (Walker, G. J., 1976, ASME J. Eng. Power, 98, pp. 229–238)

Topics: Compressors

Journal Articles

The Experimental Cascade Performance of NACA Compressor Profiles at Low Reynolds Number

W. B. Roberts

Publisher: ASME

J. Eng. Gas Turbines Power. July 1975, 97(3): 454–459.

https://doi.org/10.1115/1.3446031

Published Online: July 1, 1975

View Article titled, The Experimental Cascade Performance of NACA Compressor Profiles at Low Reynolds Number

Topics: Cascades (Fluid dynamics), Compressors, Reynolds number

Journal Articles

The Effect of Reynolds Number and Laminar Separation on Axial Cascade Performance

W. B. Roberts

Publisher: ASME

J. Eng. Gas Turbines Power. April 1975, 97(2): 261–273.

https://doi.org/10.1115/1.3445978

Published Online: April 1, 1975

View Article titled, The Effect of Reynolds Number and Laminar Separation on Axial Cascade Performance

Topics: Cascades (Fluid dynamics), Reynolds number, Separation (Technology), Bubbles, Compressors, Flow (Dynamics), Shear (Mechanics), Testing, Airfoils, Blades

Journal Articles

Closure to “Discussions of ‘The Effect of Reynolds Number and Laminar Separation on Axial Cascade Performance’” (1975, ASME J. Eng. Power, 97, pp. 273–274)

W. B. Roberts

Publisher: ASME

J. Eng. Gas Turbines Power. April 1975, 97(2): 274.

https://doi.org/10.1115/1.3445981

Published Online: April 1, 1975

View Article titled, Closure to “Discussions of ‘The Effect of Reynolds Number and Laminar Separation on Axial Cascade Performance’” (1975, ASME J. Eng. Power, 97, pp. 273–274)

Topics: Cascades (Fluid dynamics), Reynolds number, Separation (Technology)

Journal citation

NARROW

Low-Turbulence High-Speed Wind Tunnel for the Determination of Cascade Shock Losses

An Off-Design Correlation of Part Span Damper Losses Through Transonic Axial Fan Rotors

Advanced Turbofan Blade Refurbishment Technique

The Effect of Adding Roughness and Thickness to a Transonic Axial Compressor Rotor

Discussion: “The Role of Laminar-Turbulent Transition in Gas Turbine Engines” (Mayle, Robert Edward, 1991, ASME J. Turbomach., 113, pp. 509–536)

Discussion: “Similarity Behavior in Transitional Boundary Layers Over a Range of Adverse Pressure Gradients and Turbulence Levels” (Gostelow, J. P., and Walker, G. J., 1991, ASME J. Turbomach., 113, pp. 617–624)

Design Point Variation of Three-Dimensional Loss and Deviation for Axial Compressor Middle Stages

Discussion: “Secondary Flow, Turbulent Diffusion, and Mixing in Axial-Flow Compressors” (Wisler, D. C., Bauer, R. C., and Okiishi, T. H., 1987, ASME J. Turbomach., 109, pp. 455–469)

Modeling the 3-D Flow Effects on Deviation Angle for Axial Compressor Middle Stages

A Design Point Correlation for Losses due to Part-Span Dampers on Transonic Rotors

Discussion: “A Family of Surface Velocity Distributions for Axial Compressor Blading and Their Theoretical Performance” (Walker, G. J., 1976, ASME J. Eng. Power, 98, pp. 229–238)

The Experimental Cascade Performance of NACA Compressor Profiles at Low Reynolds Number

The Effect of Reynolds Number and Laminar Separation on Axial Cascade Performance

Closure to “Discussions of ‘The Effect of Reynolds Number and Laminar Separation on Axial Cascade Performance’” (1975, ASME J. Eng. Power, 97, pp. 273–274)

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