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Proceedings Papers

A Novel Centrifugal Diffuser Test Device

R. P. Shreeve, H. D. Schulz, J. R. Erwin, L. Schumann

Proc. ASME. IGT1985, Volume 1: Aircraft Engine; Turbomachinery, V001T02A049, September 1–7, 1985

Paper No: 85-IGT-135

DOI: https://doi.org/10.1115/85-IGT-135

View Paper titled, A Novel Centrifugal Diffuser Test Device

Topics: Diffusers, Flow (Dynamics), Design, Boundary layers, Cascades (Fluid dynamics), Wind tunnels

Proceedings Papers

Three-Dimensional Separated Flow Field in the Endwall Region of an Annular Compressor Cascade in the Presence of Rotor-Stator Interaction: Part I — Quasi-Steady Flow Field and Comparison With Steady-State Data

H. D. Schulz, H. E. Gallus, B. Lakshminarayana

Proc. ASME. GT1989, Volume 1: Turbomachinery, V001T01A043, June 4–8, 1989

Paper No: 89-GT-76

DOI: https://doi.org/10.1115/89-GT-76

View Paper titled, Three-Dimensional Separated Flow Field in the Endwall Region of an Annular Compressor Cascade in the Presence of Rotor-Stator Interaction: Part I — Quasi-Steady Flow Field and Comparison With Steady-State Data

Topics: Cascades (Fluid dynamics), Compressors, Flow (Dynamics), Rotors, Stators, Steady state, Blades, Boundary layers, Corners (Structural elements), Wakes

Proceedings Papers

Three-Dimensional Separated Flow Field in the Endwall Region of an Annular Compressor Cascade in the Presence of Rotor-Stator Interaction: Part II — Unsteady Flow and Pressure Field

H. D. Schulz, H. E. Gallus, B. Lakshminarayana

Proc. ASME. GT1989, Volume 1: Turbomachinery, V001T01A044, June 4–8, 1989

Paper No: 89-GT-77

DOI: https://doi.org/10.1115/89-GT-77

View Paper titled, Three-Dimensional Separated Flow Field in the Endwall Region of an Annular Compressor Cascade in the Presence of Rotor-Stator Interaction: Part II — Unsteady Flow and Pressure Field

Topics: Cascades (Fluid dynamics), Compressors, Flow (Dynamics), Pressure, Rotors, Stators, Unsteady flow, Blades, Boundary layers, Sensors

Proceedings Papers

Experimental and Numerical Investigation of Three-Dimensional Viscous Flows and Vortex Motion Inside an Annular Compressor Blade Row

H. E. Gallus, C. Hah, H. D. Schulz

Proc. ASME. GT1990, Volume 1: Turbomachinery, V001T01A051, June 11–14, 1990

Paper No: 90-GT-155

DOI: https://doi.org/10.1115/90-GT-155

View Paper titled, Experimental and Numerical Investigation of Three-Dimensional Viscous Flows and Vortex Motion Inside an Annular Compressor Blade Row

Topics: Blades, Compressors, Flow (Dynamics), Vortex motion, Boundary layers, Cascades (Fluid dynamics), Corners (Structural elements), Flow visualization, Navier-Stokes equations, Numerical analysis

Journal Articles

The Design, Fabrication, and Installation of a Quiet Compressor Station

E. Humphries, D. Schulz, J. Binek

J. Eng. Gas Turbines Power. October 1992, 114(4): 740–748.

DOI: https://doi.org/10.1115/1.2906651

Published Online: October 1, 1992

View Article titled, The Design, Fabrication, and Installation of a Quiet Compressor Station

Topics: Compressors, Design, Manufacturing, Pipelines

Journal Articles

Experimental and Numerical Investigation of Three-Dimensional Viscous Flows and Vortex Motion Inside an Annular Compressor Blade Row

H. E. Gallus, C. Hah, H. D. Schulz

J. Turbomach. April 1991, 113(2): 198–206.

DOI: https://doi.org/10.1115/1.2929083

Published Online: April 1, 1991

View Article titled, Experimental and Numerical Investigation of Three-Dimensional Viscous Flows and Vortex Motion Inside an Annular Compressor Blade Row

Topics: Blades, Compressors, Flow (Dynamics), Vortex motion, Boundary layers, Cascades (Fluid dynamics), Corners (Structural elements), Flow visualization, Numerical analysis, Pressure

Journal Articles

Three-Dimensional Separated Flow Field in the Endwall Region of an Annular Compressor Cascade in the Presence of Rotor-Stator Interaction: Part 1—Quasi-Steady Flow Field and Comparison With Steady-State Data

H. D. Schulz, H. E. Gallus, B. Lakshminarayana

J. Turbomach. October 1990, 112(4): 669–678.

DOI: https://doi.org/10.1115/1.2927707

Published Online: October 1, 1990

View Article titled, Three-Dimensional Separated Flow Field in the Endwall Region of an Annular Compressor Cascade in the Presence of Rotor-Stator Interaction: Part 1—Quasi-Steady Flow Field and Comparison With Steady-State Data

Topics: Cascades (Fluid dynamics), Compressors, Flow (Dynamics), Rotors, Stators, Steady state, Blades, Boundary layers, Corners (Structural elements), Wakes

Journal Articles

Closure to “Discussions of ‘Three-Dimensional Separated Flow Field in the Endwall Region of an Annular Compressor Cascade in the Presence of Rotor-Stator Interaction: Part 2—Unsteady Flow and Pressure Field’” (1990, ASME J. Turbomach., 112, pp. 688–689)

H. D. Schulz, H. E. Gallus, B. Lakshminarayana

J. Turbomach. October 1990, 112(4): 690.

DOI: https://doi.org/10.1115/1.2927711

Published Online: October 1, 1990

View Article titled, Closure to “Discussions of ‘Three-Dimensional Separated Flow Field in the Endwall Region of an Annular Compressor Cascade in the Presence of Rotor-Stator Interaction: Part 2—Unsteady Flow and Pressure Field’” (1990, ASME J. Turbomach., 112, pp. 688–689)

Topics: Cascades (Fluid dynamics), Compressors, Flow (Dynamics), Pressure, Rotors, Stators, Unsteady flow

Journal Articles

Three-Dimensional Separated Flow Field in the Endwall Region of an Annular Compressor Cascade in the Presence of Rotor-Stator Interaction: Part 2—Unsteady Flow and Pressure Field

H. D. Schulz, H. E. Gallus, B. Lakshminarayana

J. Turbomach. October 1990, 112(4): 679–688.

DOI: https://doi.org/10.1115/1.2927708

Published Online: October 1, 1990

View Article titled, Three-Dimensional Separated Flow Field in the Endwall Region of an Annular Compressor Cascade in the Presence of Rotor-Stator Interaction: Part 2—Unsteady Flow and Pressure Field

Topics: Cascades (Fluid dynamics), Compressors, Flow (Dynamics), Pressure, Rotors, Stators, Unsteady flow, Blades, Boundary layers, Sensors

Journal Articles

Experimental Investigation of the Three-Dimensional Flow in an Annular Compressor Cascade

H. D. Schulz, H. D. Gallus

J. Turbomach. October 1988, 110(4): 467–478.

DOI: https://doi.org/10.1115/1.3262220

Published Online: October 1, 1988

View Article titled, Experimental Investigation of the Three-Dimensional Flow in an Annular Compressor Cascade

Topics: Cascades (Fluid dynamics), Compressors, Flow (Dynamics), Blades, Boundary layers, Corners (Structural elements), Vortices, Airfoils, Flow separation, Flow visualization

Journal citation

NARROW

A Novel Centrifugal Diffuser Test Device

Three-Dimensional Separated Flow Field in the Endwall Region of an Annular Compressor Cascade in the Presence of Rotor-Stator Interaction: Part I — Quasi-Steady Flow Field and Comparison With Steady-State Data

Three-Dimensional Separated Flow Field in the Endwall Region of an Annular Compressor Cascade in the Presence of Rotor-Stator Interaction: Part II — Unsteady Flow and Pressure Field

Experimental and Numerical Investigation of Three-Dimensional Viscous Flows and Vortex Motion Inside an Annular Compressor Blade Row

The Design, Fabrication, and Installation of a Quiet Compressor Station

Experimental and Numerical Investigation of Three-Dimensional Viscous Flows and Vortex Motion Inside an Annular Compressor Blade Row

Three-Dimensional Separated Flow Field in the Endwall Region of an Annular Compressor Cascade in the Presence of Rotor-Stator Interaction: Part 1—Quasi-Steady Flow Field and Comparison With Steady-State Data

Closure to “Discussions of ‘Three-Dimensional Separated Flow Field in the Endwall Region of an Annular Compressor Cascade in the Presence of Rotor-Stator Interaction: Part 2—Unsteady Flow and Pressure Field’” (1990, ASME J. Turbomach., 112, pp. 688–689)

Three-Dimensional Separated Flow Field in the Endwall Region of an Annular Compressor Cascade in the Presence of Rotor-Stator Interaction: Part 2—Unsteady Flow and Pressure Field

Experimental Investigation of the Three-Dimensional Flow in an Annular Compressor Cascade

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