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Proceedings Papers

Stator Endwall Leading-Edge Sweep and Hub Shroud Influence on Compressor Performance

D. L. Tweedt, T. H. Okiishi, M. D. Hathaway

Proc. ASME. GT1986, Volume 1: Turbomachinery, V001T01A085, June 8–12, 1986

Paper No: 86-GT-197

DOI: https://doi.org/10.1115/86-GT-197

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Topics: Compressors, Stators, Clearances (Engineering), Blades, Aerodynamics, Axial flow

Proceedings Papers

Measurements of the Unsteady Flow Field Within the Stator Row of a Transonic Axial-Flow Fan: I — Measurement and Analysis Technique

K. L. Suder, T. H. Okiishi, M. D. Hathaway, A. J. Strazisar, J. J. Adamczyk

Proc. ASME. GT1987, Volume 1: Turbomachinery, V001T01A082, May 31–June 4, 1987

Paper No: 87-GT-226

DOI: https://doi.org/10.1115/87-GT-226

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Topics: Axial flow, Stators, Unsteady flow, Rotors, Wakes, Fluctuations (Physics), Navier-Stokes equations, Blades, Compressors, Design

Proceedings Papers

Measurements of the Unsteady Flow Field Within the Stator Row of a Transonic Axial-Flow Fan: II — Results and Discussion

M. D. Hathaway, T. H. Okiishi, K. L. Suder, A. J. Strazisar, J. J. Adamczyk

Proc. ASME. GT1987, Volume 1: Turbomachinery, V001T01A083, May 31–June 4, 1987

Paper No: 87-GT-227

DOI: https://doi.org/10.1115/87-GT-227

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Topics: Axial flow, Stators, Unsteady flow, Rotors, Wakes, Airfoils, Blades, Design, Diffusion (Physics), Fluctuations (Physics)

Proceedings Papers

NASA Low-Speed Centrifugal Compressor for 3-D Viscous Code Assessment and Fundamental Flow Physics Research

M. D. Hathaway, J. R. Wood, C. A. Wasserbauer

Proc. ASME. GT1991, Volume 1: Turbomachinery, V001T01A054, June 3–6, 1991

Paper No: 91-GT-140

DOI: https://doi.org/10.1115/91-GT-140

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Topics: Compressors, Flow (Dynamics), NASA, Physics, Computational fluid dynamics, Army, Flow visualization, Gas turbines, Laser velocimetry, Mach number

Proceedings Papers

Experimental and Computational Investigation of the NASA Low-Speed Centrifugal Compressor Flow Field

M. D. Hathaway, R. M. Chriss, J. R. Wood, A. J. Strazisar

Proc. ASME. GT1992, Volume 1: Turbomachinery, V001T01A074, June 1–4, 1992

Paper No: 92-GT-213

DOI: https://doi.org/10.1115/92-GT-213

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Topics: Compressors, Flow (Dynamics), NASA, Blades, Impellers, Lasers, Boundary layers, Computational fluid dynamics, Flow visualization, Physics

Journal Articles

Application of a Multi-Block CFD Code to Investigate the Impact of Geometry Modeling on Centrifugal Compressor Flow Field Predictions

M. D. Hathaway, J. R. Wood

J. Turbomach. October 1997, 119(4): 820–830.

DOI: https://doi.org/10.1115/1.2841193

Published Online: October 1, 1997

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Topics: Compressors, Computational fluid dynamics, Flow (Dynamics), Geometry, Modeling, Clearances (Engineering), Impellers, Lasers, NASA, Clocks

Journal Articles

Experimental and Computational Results From the NASA Lewis Low-Speed Centrifugal Impeller at Design and Part-Flow Conditions

R. M. Chriss, M. D. Hathaway, J. R. Wood

J. Turbomach. January 1996, 118(1): 55–65.

DOI: https://doi.org/10.1115/1.2836607

Published Online: January 1, 1996

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Topics: Design, Flow (Dynamics), Impellers, NASA, Blades, Clearances (Engineering), Wakes, Boundary layers, Compressors, Lasers

Journal Articles

Closure to “Discussion of ‘Experimental and Computational Investigation of the NASA Low-Speed Centrifugal Compressor Flow Field’” (1993, ASME J. Turbomach., 115, pp. 541–542)

M. D. Hathaway, R. M. Chriss, J. R. Wood, A. J. Strazisar

J. Turbomach. July 1993, 115(3): 542.

DOI: https://doi.org/10.1115/1.2929287

Published Online: July 1, 1993

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Topics: Compressors, Flow (Dynamics), NASA

Journal Articles

Experimental and Computational Investigation of the NASA Low-Speed Centrifugal Compressor Flow Field

M. D. Hathaway, R. M. Chriss, J. R. Wood, A. J. Strazisar

J. Turbomach. July 1993, 115(3): 527–541.

DOI: https://doi.org/10.1115/1.2929285

Published Online: July 1, 1993

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Topics: Compressors, Flow (Dynamics), NASA, Blades, Impellers, Lasers, Boundary layers, Computational fluid dynamics, Flow visualization, Physics

Journal Articles

NASA Low-Speed Centrifugal Compressor for Three-Dimensional Viscous Code Assessment and Fundamental Flow Physics Research

M. D. Hathaway, J. R. Wood, C. A. Wasserbauer

J. Turbomach. April 1992, 114(2): 295–303.

DOI: https://doi.org/10.1115/1.2929143

Published Online: April 1, 1992

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Topics: Compressors, Flow (Dynamics), NASA, Physics, Computational fluid dynamics, Army, Flow visualization, Gas turbines, Laser velocimetry, Mach number

Journal Articles

Closure to “Discussion of ‘Stator Endwall Leading-Edge Sweep and Hub Shroud Influence on Compressor Performance’” (1987, ASME J. Turbomach., 109, pp. 310–311)

D. L. Tweedt, T. H. Okiishi, M. D. Hathaway

J. Turbomach. April 1987, 109(2): 311.

DOI: https://doi.org/10.1115/1.3262107

Published Online: April 1, 1987

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Topics: Compressors, Stators

Journal Articles

Stator Endwall Leading-Edge Sweep and Hub Shroud Influence on Compressor Performance

D. L. Tweedt, T. H. Okiishi, M. D. Hathaway

J. Turbomach. October 1986, 108(2): 224–232.

DOI: https://doi.org/10.1115/1.3262041

Published Online: October 1, 1986

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Topics: Compressors, Stators, Clearances (Engineering), Blades, Aerodynamics, Axial flow

Journal Articles

A Note on Blade Wake Interaction Influence on Compressor Stator Row Aerodynamic Performance

T. H. Okiishi, M. D. Hathaway, J. L. Hansen

J. Eng. Gas Turbines Power. April 1985, 107(2): 549–551.

DOI: https://doi.org/10.1115/1.3239768

Published Online: April 1, 1985

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Topics: Blades, Compressors, Stators, Wakes

Journal citation

NARROW

Stator Endwall Leading-Edge Sweep and Hub Shroud Influence on Compressor Performance

Measurements of the Unsteady Flow Field Within the Stator Row of a Transonic Axial-Flow Fan: I — Measurement and Analysis Technique

Measurements of the Unsteady Flow Field Within the Stator Row of a Transonic Axial-Flow Fan: II — Results and Discussion

NASA Low-Speed Centrifugal Compressor for 3-D Viscous Code Assessment and Fundamental Flow Physics Research

Experimental and Computational Investigation of the NASA Low-Speed Centrifugal Compressor Flow Field

Application of a Multi-Block CFD Code to Investigate the Impact of Geometry Modeling on Centrifugal Compressor Flow Field Predictions

Experimental and Computational Results From the NASA Lewis Low-Speed Centrifugal Impeller at Design and Part-Flow Conditions

Closure to “Discussion of ‘Experimental and Computational Investigation of the NASA Low-Speed Centrifugal Compressor Flow Field’” (1993, ASME J. Turbomach., 115, pp. 541–542)

Experimental and Computational Investigation of the NASA Low-Speed Centrifugal Compressor Flow Field

NASA Low-Speed Centrifugal Compressor for Three-Dimensional Viscous Code Assessment and Fundamental Flow Physics Research

Closure to “Discussion of ‘Stator Endwall Leading-Edge Sweep and Hub Shroud Influence on Compressor Performance’” (1987, ASME J. Turbomach., 109, pp. 310–311)

Stator Endwall Leading-Edge Sweep and Hub Shroud Influence on Compressor Performance

A Note on Blade Wake Interaction Influence on Compressor Stator Row Aerodynamic Performance

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