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Proceedings Papers

Three-Dimensional Flowfields Inside a Transonic Compressor With Swept Blades

C. Hah, A. J. Wennerstrom

Proc. ASME. GT1990, Volume 1: Turbomachinery, V001T01A107, June 11–14, 1990

Paper No: 90-GT-359

DOI: https://doi.org/10.1115/90-GT-359

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Topics: Blades, Compressors, Rotors, Flow (Dynamics), Shock (Mechanics), Turbulence, Clearances (Engineering), Modeling, Navier-Stokes equations, Relaxation (Physics)

Proceedings Papers

Wake Mixing Improvements in a Linear Compressor Cascade With Crenulated Trailing Edges

J. L. Veesart, P. I. King, W. C. Elrod, A. J. Wennerstrom

Proc. ASME. GT1990, Volume 5: Manufacturing Materials and Metallurgy; Ceramics; Structures and Dynamics; Controls, Diagnostics and Instrumentation; General, V005T16A009, June 11–14, 1990

Paper No: 90-GT-218

DOI: https://doi.org/10.1115/90-GT-218

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Topics: Cascades (Fluid dynamics), Compressors, Wakes, Pressure, Blades, Energy dissipation, Flow turning, Gas turbines, Suction, Vortices

Journal Articles

A Three-Dimensional Shock Loss Model Applied to an Aft-Swept, Transonic Compressor Rotor

S. L. Puterbaugh, W. W. Copenhaver, C. Hah, A. J. Wennerstrom

J. Turbomach. July 1997, 119(3): 452–459.

DOI: https://doi.org/10.1115/1.2841144

Published Online: July 1, 1997

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Topics: Compressors, Rotors, Shock (Mechanics), Design, Flow (Dynamics), Geometry, Pressure, Airfoils, Design methodology

Journal Articles

Closure to “Discussion of ‘Three-Dimensional Flowfields Inside a Transonic Compressor With Swept Blades’” (1991, ASME J. Turbomach., 113, pp. 250–251)

C. Hah, A. J. Wennerstrom

J. Turbomach. April 1991, 113(2): 251.

DOI: https://doi.org/10.1115/1.2929094

Published Online: April 1, 1991

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Topics: Compressors

Journal Articles

A Review of Predictive Efforts for Transport Phenomena in Axial Flow Compressors

A. J. Wennerstrom

J. Turbomach. April 1991, 113(2): 175–179.

DOI: https://doi.org/10.1115/1.2929080

Published Online: April 1, 1991

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Topics: Axial flow, Compressors, Transport phenomena, Flow (Dynamics), Turbulence

Journal Articles

Three-Dimensional Flowfields Inside a Transonic Compressor With Swept Blades

C. Hah, A. J. Wennerstrom

J. Turbomach. April 1991, 113(2): 241–250.

DOI: https://doi.org/10.1115/1.2929092

Published Online: April 1, 1991

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Topics: Blades, Compressors, Rotors, Flow (Dynamics), Shock (Mechanics), Turbulence, Clearances (Engineering), Modeling, Relaxation (Physics), Reynolds number

Journal Articles

Highly Loaded Axial Flow Compressors: History and Current Developments

A. J. Wennerstrom

J. Turbomach. October 1990, 112(4): 567–578.

DOI: https://doi.org/10.1115/1.2927695

Published Online: October 1, 1990

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Topics: Axial flow, Compressors, Diffusion (Physics), Mach number, Aircraft, Gas turbines, Power stations, Weight (Mass)

Journal Articles

Low Aspect Ratio Axial Flow Compressors: Why and What It Means

A. J. Wennerstrom

J. Turbomach. October 1989, 111(4): 357–365.

DOI: https://doi.org/10.1115/1.3262280

Published Online: October 1, 1989

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Topics: Axial flow, Compressors, Design, Aircraft, Design engineering, Engines, Gas turbines, Fans, Pendulums, Stability

Journal Articles

Characterization of Shock Wave–Endwall Boundary Layer Interactions in a Transonic Compressor Rotor

D. C. Rabe, A. J. Wennerstrom, W. F. O’Brien

J. Turbomach. July 1988, 110(3): 386–392.

DOI: https://doi.org/10.1115/1.3262208

Published Online: July 1, 1988

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Topics: Boundary layers, Compressors, Rotors, Shock waves, Blades, Lasers, Air Force, Chords (Trusses), Flow (Dynamics), Shear (Mechanics)

Journal Articles

Some Experiments With a Supersonic Axial Compressor Stage

A. J. Wennerstrom

J. Turbomach. July 1987, 109(3): 388–397.

DOI: https://doi.org/10.1115/1.3262118

Published Online: July 1, 1987

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Topics: Compressors, Design, Rotors, Flow (Dynamics), Pressure, Boundary layers, Generators, Vortices, Diffusion (Physics), Geometry

Journal Articles

Thermodynamics and Fluid Mechanics of Turbomachinery

A. S. Ucer, Editor, P. Stow, Editor, C. Hirsch, Editor, A. J. Wennerstrom, Reviewer

J. Turbomach. July 1987, 109(3): 453.

DOI: https://doi.org/10.1115/1.3262126

Published Online: July 1, 1987

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Topics: Fluid mechanics, Thermodynamics, Turbomachinery

Journal Articles

Discussion: “Stator Endwall Leading-Edge Sweep and Hub Shroud Influence on Compressor Performance” (Tweedt, D. L., Okiishi, T. H., and Hathaway, M. D., 1986, ASME J. Turbomach., 108, pp. 224–232)

A. J. Wennerstrom

J. Turbomach. April 1987, 109(2): 310–311.

DOI: https://doi.org/10.1115/1.3262106

Published Online: April 1, 1987

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Topics: Compressors, Stators

Journal Articles

Performance of Two Transonic Axial Compressor Rotors Incorporating Inlet Counterswirl

C. H. Law, A. J. Wennerstrom

J. Turbomach. January 1987, 109(1): 142–148.

DOI: https://doi.org/10.1115/1.3262059

Published Online: January 1, 1987

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Topics: Compressors, Rotors, Blades, Design, Shock (Mechanics), Pressure, Axial flow, Computation, Diffusion (Physics), Flow (Dynamics)

Journal Articles

Experimental Study of a High-Throughflow Transonic Axial Compressor Stage

A. J. Wennerstrom

J. Eng. Gas Turbines Power. July 1984, 106(3): 552–560.

DOI: https://doi.org/10.1115/1.3239606

Published Online: July 1, 1984

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Topics: Compressors, Design, Generators, Rotors, Vortices, Pressure

Journal Articles

A Three-Dimensional Model for the Prediction of Shock Losses in Compressor Blade Rows

A. J. Wennerstrom, S. L. Puterbaugh

J. Eng. Gas Turbines Power. April 1984, 106(2): 295–299.

DOI: https://doi.org/10.1115/1.3239562

Published Online: April 1, 1984

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Topics: Blades, Compressors, Shock (Mechanics), Three-dimensional models, Aircraft, Design, Fans, Flow (Dynamics), Gas turbines, Turbines

Journal Articles

On Predicting Flow Through Porous Media

R. L. Haugen, A. J. Wennerstrom

J. Appl. Mech. December 1970, 37(4): 1179–1180.

DOI: https://doi.org/10.1115/1.3408688

Published Online: December 1, 1970

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Topics: Flow (Dynamics), Porous materials

Journal citation

NARROW

Three-Dimensional Flowfields Inside a Transonic Compressor With Swept Blades

Wake Mixing Improvements in a Linear Compressor Cascade With Crenulated Trailing Edges

A Three-Dimensional Shock Loss Model Applied to an Aft-Swept, Transonic Compressor Rotor

Closure to “Discussion of ‘Three-Dimensional Flowfields Inside a Transonic Compressor With Swept Blades’” (1991, ASME J. Turbomach., 113, pp. 250–251)

A Review of Predictive Efforts for Transport Phenomena in Axial Flow Compressors

Three-Dimensional Flowfields Inside a Transonic Compressor With Swept Blades

Highly Loaded Axial Flow Compressors: History and Current Developments

Low Aspect Ratio Axial Flow Compressors: Why and What It Means

Characterization of Shock Wave–Endwall Boundary Layer Interactions in a Transonic Compressor Rotor

Some Experiments With a Supersonic Axial Compressor Stage

Thermodynamics and Fluid Mechanics of Turbomachinery

Discussion: “Stator Endwall Leading-Edge Sweep and Hub Shroud Influence on Compressor Performance” (Tweedt, D. L., Okiishi, T. H., and Hathaway, M. D., 1986, ASME J. Turbomach., 108, pp. 224–232)

Performance of Two Transonic Axial Compressor Rotors Incorporating Inlet Counterswirl

Experimental Study of a High-Throughflow Transonic Axial Compressor Stage

A Three-Dimensional Model for the Prediction of Shock Losses in Compressor Blade Rows

On Predicting Flow Through Porous Media

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