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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

Proceedings Papers

Laser Anemometer Measurements of the Flow Field in a 4:1 Pressure Ratio Centrifugal Impeller

G. J. Skoch, P. S. Prahst, M. P. Wernet, J. R. Wood, A. J. Strazisar

Proc. ASME. GT1997, Volume 1: Aircraft Engine; Marine; Turbomachinery; Microturbines and Small Turbomachinery, V001T03A049, June 2–5, 1997

Paper No: 97-GT-342

DOI: https://doi.org/10.1115/97-GT-342

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Topics: Flow (Dynamics), Impellers, Lasers, Pressure, Blades, Clearances (Engineering), Suction, Vaneless diffusers, Chords (Trusses), Computational fluid dynamics

Proceedings Papers

On Flowfield Periodicity in the NASA Transonic Flutter Cascade: Part I — Experimental Study

J. Lepicovsky, E. R. McFarland, R. V. Chima, J. R. Wood

Proc. ASME. GT2000, Volume 1: Aircraft Engine; Marine; Turbomachinery; Microturbines and Small Turbomachinery, V001T03A097, May 8–11, 2000

Paper No: 2000-GT-0572

DOI: https://doi.org/10.1115/2000-GT-0572

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Topics: Cascades (Fluid dynamics), Flutter (Aerodynamics), NASA, Blades, Flow (Dynamics), Boundary layers, Stress, Tunnels, Data acquisition, Geometry

Proceedings Papers

On Flowfield Periodicity in the NASA Transonic Flutter Cascade: Part II — Numerical Study

R. V. Chima, E. R. McFarland, J. R. Wood, J. Lepicovsky

Proc. ASME. GT2000, Volume 1: Aircraft Engine; Marine; Turbomachinery; Microturbines and Small Turbomachinery, V001T03A098, May 8–11, 2000

Paper No: 2000-GT-0573

DOI: https://doi.org/10.1115/2000-GT-0573

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Topics: Cascades (Fluid dynamics), Flutter (Aerodynamics), NASA, Blades, Computational fluid dynamics, Boundary layers, Flow (Dynamics), Numerical analysis, Paints, Pressure

Journal Articles

On Flowfield Periodicity in the NASA Transonic Flutter Cascade

J. Lepicovsky, R. V. Chima, E. R. McFarland, J. R. Wood

J. Turbomach. July 2001, 123(3): 501–509.

DOI: https://doi.org/10.1115/1.1378300

Published Online: February 1, 2000

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Topics: Blades, Cascades (Fluid dynamics), Flow (Dynamics), Pressure, Flutter (Aerodynamics), Boundary layers

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

Application of Advanced Computational Codes in the Design of an Experiment for a Supersonic Throughflow Fan Rotor

J. R. Wood, J. F. Schmidt, R. J. Steinke, R. V. Chima, W. G. Kunik

J. Turbomach. April 1988, 110(2): 270–279.

DOI: https://doi.org/10.1115/1.3262191

Published Online: April 1, 1988

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Topics: Design, Rotors, Blades, Mach number, Nozzles, Boundary layers, Flow (Dynamics), Shapes, Axial flow, Databases

Journal Articles

Effect of Area Ratio on the Performance of a 5.5:1 Pressure Ratio Centrifugal Impeller

L. F. Schumann, D. A. Clark, J. R. Wood

J. Turbomach. January 1987, 109(1): 10–19.

DOI: https://doi.org/10.1115/1.3262055

Published Online: January 1, 1987

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Topics: Impellers, Pressure, Design, Clearances (Engineering), Flow (Dynamics), Separation (Technology), Blades, Computers, Cutting, Diffusion (Physics)

Journal Articles

Closure to “Discussions of ‘Investigation of the Three-Dimensional Flow Field Within a Transonic Fan Rotor: Experiment and Analysis’” (1985, ASME J. Eng. Gas Turbines Power, 107, p. 448)

M. J. Pierzga, J. R. Wood

J. Eng. Gas Turbines Power. April 1985, 107(2): 449.

DOI: https://doi.org/10.1115/1.3239747

Published Online: April 1, 1985

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Topics: Flow (Dynamics), Gas turbines, Rotors

Journal Articles

Investigation of the Three-Dimensional Flow Field Within a Transonic Fan Rotor: Experiment and Analysis

M. J. Pierzga, J. R. Wood

J. Eng. Gas Turbines Power. April 1985, 107(2): 436–448.

DOI: https://doi.org/10.1115/1.3239744

Published Online: April 1, 1985

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Topics: Flow (Dynamics), Rotors, Blades, Design, Lasers, Axial flow, Boundary layers, Mach number, Numerical analysis, Pressure

Journal Articles

Discussion: “Detailed Flow Investigations Within a High-Speed Centrifugal Compressor Impeller” (Eckardt, D., 1976, ASME J. Fluids Eng., 98, pp. 390–399)

J. R. Wood

J. Fluids Eng. September 1976, 98(3): 399.

DOI: https://doi.org/10.1115/1.3448336

Published Online: September 1, 1976

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Topics: Compressor impellers, Flow (Dynamics), Fluids

Journal citation

NARROW

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

Laser Anemometer Measurements of the Flow Field in a 4:1 Pressure Ratio Centrifugal Impeller

On Flowfield Periodicity in the NASA Transonic Flutter Cascade: Part I — Experimental Study

On Flowfield Periodicity in the NASA Transonic Flutter Cascade: Part II — Numerical Study

On Flowfield Periodicity in the NASA Transonic Flutter Cascade

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

Application of Advanced Computational Codes in the Design of an Experiment for a Supersonic Throughflow Fan Rotor

Effect of Area Ratio on the Performance of a 5.5:1 Pressure Ratio Centrifugal Impeller

Closure to “Discussions of ‘Investigation of the Three-Dimensional Flow Field Within a Transonic Fan Rotor: Experiment and Analysis’” (1985, ASME J. Eng. Gas Turbines Power, 107, p. 448)

Investigation of the Three-Dimensional Flow Field Within a Transonic Fan Rotor: Experiment and Analysis

Discussion: “Detailed Flow Investigations Within a High-Speed Centrifugal Compressor Impeller” (Eckardt, D., 1976, ASME J. Fluids Eng., 98, pp. 390–399)

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