Search Results | ASME Digital Collection

1-9 of 9

Sort by

Sort Order Select

Proceedings Papers

The Combined Effect of Axial Velocity Density Ratio and Aspect Ratio on Compressor Cascade Performance

U. Stark, H. Hoheisel

Proc. ASME. GT1980, Volume 1B: General, V01BT02A044, March 10–13, 1980

Paper No: 80-GT-138

DOI: https://doi.org/10.1115/80-GT-138

View Paper titled, The Combined Effect of Axial Velocity Density Ratio and Aspect Ratio on Compressor Cascade Performance

Topics: Cascades (Fluid dynamics), Compressors, Density, Compressible flow, Pressure, Shapes, Turning angles

Proceedings Papers

A Numerical Investigation of the Effect of End-Wall Boundary Layer Skew on the Aerodynamic Performance of a Low Aspect Ratio, High Turning Compressor Cascade

M. Boehle, U. Stark

Proc. ASME. IMECE2007, Volume 8: Heat Transfer, Fluid Flows, and Thermal Systems, Parts A and B, 555-564, November 11–15, 2007

Paper No: IMECE2007-44049

DOI: https://doi.org/10.1115/IMECE2007-44049

View Paper titled, A Numerical Investigation of the Effect of End-Wall Boundary Layer Skew on the Aerodynamic Performance of a Low Aspect Ratio, High Turning Compressor Cascade

Topics: Boundary layers, Cascades (Fluid dynamics), Compressors, Turning, Blades, Flow (Dynamics), Suction, Turbulence, Axial flow, Chords (Trusses)

Proceedings Papers

Structure of the Rotor Tip Flow in a Highly Loaded Single-Stage Axial-Flow Pump Approaching Stall: Part II — Stall Inception — Understanding the Mechanism and Overcoming Its Negative Impacts

I. Goltz, G. Kosyna, D. Wulff, H. Schrapp, U. Stark, H. Saathoff, S. Bross

Proc. ASME. HT-FED2004, Volume 3, 301-306, July 11–15, 2004

Paper No: HT-FED2004-56770

DOI: https://doi.org/10.1115/HT-FED2004-56770

View Paper titled, Structure of the Rotor Tip Flow in a Highly Loaded Single-Stage Axial-Flow Pump Approaching Stall: Part II — Stall Inception — Understanding the Mechanism and Overcoming Its Negative Impacts

Topics: Axial flow, Flow (Dynamics), Pumps, Rotors, Stall inception

Proceedings Papers

Structure of the Rotor Tip Flow in a Highly-Loaded Single-Stage Axial-Flow Pump Approaching Stall: Part I — Breakdown of the Tip-Clearance Vortex

H. Schrapp, U. Stark, I. Goltz, G. Kosyna, S. Bross

Proc. ASME. HT-FED2004, Volume 3, 307-312, July 11–15, 2004

Paper No: HT-FED2004-56780

DOI: https://doi.org/10.1115/HT-FED2004-56780

View Paper titled, Structure of the Rotor Tip Flow in a Highly-Loaded Single-Stage Axial-Flow Pump Approaching Stall: Part I — Breakdown of the Tip-Clearance Vortex

Topics: Axial flow, Clearances (Engineering), Flow (Dynamics), Pumps, Rotors, Vortices, Boundary-value problems, Cavitation, Design, Pressure

Proceedings Papers

Flow Structure of an Axial-Flow Pump From Stable Operation to Deep Stall

G. Kosyna, I. Goltz, U. Stark

Proc. ASME. FEDSM2005, Volume 1: Symposia, Parts A and B, 1389-1396, June 19–23, 2005

Paper No: FEDSM2005-77350

DOI: https://doi.org/10.1115/FEDSM2005-77350

View Paper titled, Flow Structure of an Axial-Flow Pump From Stable Operation to Deep Stall

Topics: Axial flow, Flow (Dynamics), Pumps, Stall inception, Vortices

Journal Articles

Discussion: “Criteria for Spike Initiated Rotating Stall” ( Vo, H. D., Tan, C. S., Greitzer, E. M., 2008, ASME J. Turbomach., 130, p. 011023 )

A. Deppe, H. Saathoff, U. Stark

J. Turbomach. January 2008, 130(1): 015501.

DOI: https://doi.org/10.1115/1.2750673

Published Online: January 30, 2008

View Article titled, Discussion: “Criteria for Spike Initiated Rotating Stall” ( Vo, H. D., Tan, C. S., Greitzer, E. M., 2008, ASME J. Turbomach., 130, p. 011023 )

Topics: Compressors, Rotors, Stall inception, Pressure, Flow (Dynamics), Blades

Journal Articles

The Combined Effect of Axial Velocity Density Ratio and Aspect Ratio on Compressor Cascade Performance

U. Stark, H. Hoheisel

J. Eng. Gas Turbines Power. January 1981, 103(1): 247–255.

DOI: https://doi.org/10.1115/1.3230704

Published Online: January 1, 1981

View Article titled, The Combined Effect of Axial Velocity Density Ratio and Aspect Ratio on Compressor Cascade Performance

Topics: Cascades (Fluid dynamics), Compressors, Density, Compressible flow, Pressure, Shapes, Turning angles

Journal Articles

Discussion: “Deviation Angle Estimation for Axial-Flow Compressors Using Inviscid Flow Solutions” (Miller, M. J., and Serovy, G. K., 1975, ASME J. Eng. Power, 97, pp. 163–168)

U. Stark, J. Starke

J. Eng. Gas Turbines Power. April 1975, 97(2): 170–172.

DOI: https://doi.org/10.1115/1.3445949

Published Online: April 1, 1975

View Article titled, Discussion: “Deviation Angle Estimation for Axial-Flow Compressors Using Inviscid Flow Solutions” (Miller, M. J., and Serovy, G. K., 1975, ASME J. Eng. Power, 97, pp. 163–168)

Topics: Axial flow, Compressors, Inviscid flow

Journal Articles

A Theoretical Investigation of the Jet-Flap Compressor Cascade in Incompressible Flow

U. Stark

J. Eng. Gas Turbines Power. October 1972, 94(4): 249–260.

DOI: https://doi.org/10.1115/1.3445680

Published Online: October 1, 1972

View Article titled, A Theoretical Investigation of the Jet-Flap Compressor Cascade in Incompressible Flow

Topics: Cascades (Fluid dynamics), Compressors, Flow (Dynamics), Turning angles, Blades, Flat plates, Inviscid flow, Pressure

Journal citation

NARROW

The Combined Effect of Axial Velocity Density Ratio and Aspect Ratio on Compressor Cascade Performance

A Numerical Investigation of the Effect of End-Wall Boundary Layer Skew on the Aerodynamic Performance of a Low Aspect Ratio, High Turning Compressor Cascade

Structure of the Rotor Tip Flow in a Highly Loaded Single-Stage Axial-Flow Pump Approaching Stall: Part II — Stall Inception — Understanding the Mechanism and Overcoming Its Negative Impacts

Structure of the Rotor Tip Flow in a Highly-Loaded Single-Stage Axial-Flow Pump Approaching Stall: Part I — Breakdown of the Tip-Clearance Vortex

Flow Structure of an Axial-Flow Pump From Stable Operation to Deep Stall

Discussion: “Criteria for Spike Initiated Rotating Stall” ( Vo, H. D., Tan, C. S., Greitzer, E. M., 2008, ASME J. Turbomach., 130, p. 011023 )

The Combined Effect of Axial Velocity Density Ratio and Aspect Ratio on Compressor Cascade Performance

Discussion: “Deviation Angle Estimation for Axial-Flow Compressors Using Inviscid Flow Solutions” (Miller, M. J., and Serovy, G. K., 1975, ASME J. Eng. Power, 97, pp. 163–168)

A Theoretical Investigation of the Jet-Flap Compressor Cascade in Incompressible Flow

Journals

Conference Proceedings

eBooks

Resources

Opportunities

Journals

Conference Proceedings

eBooks

Resources

Opportunities

This Feature Is Available To Subscribers Only