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Proceedings Papers

Supersonic Exit Flow of Two-Dimensional Cascades

Proc. ASME. GT1972, ASME 1972 International Gas Turbine and Fluids Engineering Conference and Products Show, V001T01A048, March 26–30, 1972

Publisher: American Society of Mechanical Engineers

Paper No: 72-GT-49

https://doi.org/10.1115/72-GT-49

View Paper titled, Supersonic Exit Flow of Two-Dimensional Cascades

Topics: Flow (Dynamics), Cascades (Fluid dynamics), Computational methods, Pressure

Proceedings Papers

Design and Testing of Two Supercritical Compressor Cascades

H. Rechter, P. Schimming, H. Starken

Proc. ASME. GT1979, Volume 1A: Gas Turbines, V01AT01A011, March 12–15, 1979

Publisher: American Society of Mechanical Engineers

Paper No: 79-GT-11

https://doi.org/10.1115/79-GT-11

View Paper titled, Design and Testing of Two Supercritical Compressor Cascades

Topics: Compressors, Design, Testing, Blades, Cascades (Fluid dynamics), Pressure, Flow (Dynamics), Boundary layers, Flow turning, Mach number

Proceedings Papers

Supersonic Cascade Interaction

H. J. Lichtfuss, H. Starken

Proc. ASME. GT1974, Volume 1A: General, V01AT01A076, March 30–April 4, 1974

Publisher: American Society of Mechanical Engineers

Paper No: 74-GT-76

https://doi.org/10.1115/74-GT-76

View Paper titled, Supersonic Cascade Interaction

Topics: Cascades (Fluid dynamics), Flow (Dynamics), Blades, Flat plates, Supersonic flow

Proceedings Papers

Investigation of the Axial Velocity Density Ratio in a High Turning Cascade

H. Starken, F. A. E. Breugelmans, P. Schimming

Proc. ASME. GT1975, Volume 1A: General, V01AT01A024, March 2–6, 1975

Publisher: American Society of Mechanical Engineers

Paper No: 75-GT-25

https://doi.org/10.1115/75-GT-25

View Paper titled, Investigation of the Axial Velocity Density Ratio in a High Turning Cascade

Topics: Cascades (Fluid dynamics), Density, Turning, Blades, Flow (Dynamics), Stators, Mach number

Proceedings Papers

Experimental Investigations of Supersonic Cascades Designed for High Static Pressure Ratios

R. Fuchs, H. Starken

Proc. ASME. GT1977, ASME 1977 International Gas Turbine Conference and Products Show, V001T01A036, March 27–31, 1977

Publisher: American Society of Mechanical Engineers

Paper No: 77-GT-37

https://doi.org/10.1115/77-GT-37

View Paper titled, Experimental Investigations of Supersonic Cascades Designed for High Static Pressure Ratios

Topics: Pressure, Cascades (Fluid dynamics), Blades, Design, Flow turning, Rotors, Boundary layers, Compressors, Impulse (Physics), Mach number

Proceedings Papers

Redesign and Performance Analysis of a Transonic Axial Compressor Stator and Equivalent Plane Cascades With Subsonic Controlled Diffusion Blades

R. Dunker, H. Rechter, H. Starken, H. Weyer

Proc. ASME. GT1983, Volume 1: Turbomachinery, V001T01A055, March 27–31, 1983

Publisher: American Society of Mechanical Engineers

Paper No: 83-GT-208

https://doi.org/10.1115/83-GT-208

View Paper titled, Redesign and Performance Analysis of a Transonic Axial Compressor Stator and Equivalent Plane Cascades With Subsonic Controlled Diffusion Blades

Topics: Blades, Compressors, Diffusion (Physics), Stators, Design, Cascades (Fluid dynamics), Flow (Dynamics), Pressure, Boundary layers, Density

Proceedings Papers

Experimental Cascade Analysis of a Transonic Compressor Rotor Blade Section

H. A. Schreiber, H. Starken

Proc. ASME. GT1983, Volume 1: Turbomachinery, V001T01A056, March 27–31, 1983

Publisher: American Society of Mechanical Engineers

Paper No: 83-GT-209

https://doi.org/10.1115/83-GT-209

View Paper titled, Experimental Cascade Analysis of a Transonic Compressor Rotor Blade Section

Topics: Blades, Cascades (Fluid dynamics), Compressors, Rotors, Flow (Dynamics), Axial flow, Density, Design, Mach number, Shock (Mechanics)

Proceedings Papers

Theoretical and Experimental Analysis of a Compressor Cascade at Supercritical Flow Conditions

A. Weber, M. Faden, H. Starken, V. Jawtusch

Proc. ASME. GT1987, Volume 1: Turbomachinery, V001T01A099, May 31–June 4, 1987

Publisher: American Society of Mechanical Engineers

Paper No: 87-GT-256

https://doi.org/10.1115/87-GT-256

View Paper titled, Theoretical and Experimental Analysis of a Compressor Cascade at Supercritical Flow Conditions

Topics: Cascades (Fluid dynamics), Compressors, Experimental analysis, Flow (Dynamics), Boundary layers, Blades, Displacement, Finite element methods, Mach number, Metals

Proceedings Papers

Design and Testing of a Controlled Diffusion Airfoil Cascade for Industrial Axial Flow Compressor Application

W. Steinert, B. Eisenberg, H. Starken

Proc. ASME. GT1990, Volume 1: Turbomachinery, V001T01A044, June 11–14, 1990

Publisher: American Society of Mechanical Engineers

Paper No: 90-GT-140

https://doi.org/10.1115/90-GT-140

View Paper titled, Design and Testing of a Controlled Diffusion Airfoil Cascade for Industrial Axial Flow Compressor Application

Topics: Airfoils, Axial flow, Cascades (Fluid dynamics), Design, Diffusion (Physics), Testing, Compressors, Blades, Boundary layers, Computational methods

Proceedings Papers

An Investigation of a Strong Shock-Wave Turbulent Boundary Layer Interaction in a Supersonic Compressor Cascade

H. A. Schreiber, H. Starken

Proc. ASME. GT1991, Volume 1: Turbomachinery, V001T01A040, June 3–6, 1991

Publisher: American Society of Mechanical Engineers

Paper No: 91-GT-092

https://doi.org/10.1115/91-GT-092

View Paper titled, An Investigation of a Strong Shock-Wave Turbulent Boundary Layer Interaction in a Supersonic Compressor Cascade

Topics: Boundary layer turbulence, Cascades (Fluid dynamics), Compressors, Shock waves, Blades, Mach number, Pressure, Shock (Mechanics), Boundary layers, Chords (Trusses)

Proceedings Papers

Design and Analysis of a High Pitch to Chord Ratio Cascade Representative of Ducted Propfans

A. Weber, W. Steinert, H. Starken

Proc. ASME. GT1991, Volume 1: Turbomachinery, V001T01A101, June 3–6, 1991

Publisher: American Society of Mechanical Engineers

Paper No: 91-GT-335

https://doi.org/10.1115/91-GT-335

View Paper titled, Design and Analysis of a High Pitch to Chord Ratio Cascade Representative of Ducted Propfans

Topics: Cascades (Fluid dynamics), Chords (Trusses), Design, Blades, Mach number, Boundary layers, Pressure, Aircraft engines, Flow (Dynamics), Flow turning

Proceedings Papers

Inlet Flow Angle Determination of Transonic Compressor Cascades

W. Steinert, R. Fuchs, H. Starken

Proc. ASME. GT1991, Volume 1: Turbomachinery, V001T01A086, June 3–6, 1991

Publisher: American Society of Mechanical Engineers

Paper No: 91-GT-274

https://doi.org/10.1115/91-GT-274

View Paper titled, Inlet Flow Angle Determination of Transonic Compressor Cascades

Topics: Compressors, Flow (Dynamics), Mach number, Suction, Testing

Proceedings Papers

Transonic Compressor Rotor Cascade With Boundary-Layer Separation: Experimental and Theoretical Results

R. Fuchs, W. Steinert, H. Starken

Proc. ASME. GT1993, Volume 3C: General, V03CT17A066, May 24–27, 1993

Publisher: American Society of Mechanical Engineers

Paper No: 93-GT-405

https://doi.org/10.1115/93-GT-405

View Paper titled, Transonic Compressor Rotor Cascade With Boundary-Layer Separation: Experimental and Theoretical Results

Topics: Boundary layers, Cascades (Fluid dynamics), Compressors, Rotors, Separation (Technology), Design, Mach number, Bubbles, Flow (Dynamics), Blades

Journal Articles

Off-Design Transition and Separation Behavior of a CDA Cascade

W. Steinert, H. Starken

Publisher: ASME

J. Turbomach. April 1996, 118(2): 204–210.

https://doi.org/10.1115/1.2836627

Published Online: April 1, 1996

View Article titled, Off-Design Transition and Separation Behavior of a CDA Cascade

Topics: Cascades (Fluid dynamics), Design, Separation (Technology), Blades, Airfoils, Axial flow, Boundary layers, Compressors, Diffusion (Physics), Inks

Journal Articles

An Investigation of a Strong Shock-Wave Turbulent Boundary Layer Interaction in a Supersonic Compressor Cascade

H. A. Schreiber, H. Starken

Publisher: ASME

J. Turbomach. July 1992, 114(3): 494–503.

https://doi.org/10.1115/1.2929170

Published Online: July 1, 1992

View Article titled, An Investigation of a Strong Shock-Wave Turbulent Boundary Layer Interaction in a Supersonic Compressor Cascade

Topics: Boundary layer turbulence, Cascades (Fluid dynamics), Compressors, Shock waves, Blades, Mach number, Pressure, Boundary layers, Chords (Trusses), Density

Journal Articles

Closure to “Discussion of ‘An Investigation of a Strong Shock-Wave Turbulent Boundary Layer Interaction in a Supersonic Compressor Cascade’” (1992, ASME J. Turbomach., 114, p. 503)

H. A. Schreiber, H. Starken

Publisher: ASME

J. Turbomach. July 1992, 114(3): 503.

https://doi.org/10.1115/1.2929172

Published Online: July 1, 1992

View Article titled, Closure to “Discussion of ‘An Investigation of a Strong Shock-Wave Turbulent Boundary Layer Interaction in a Supersonic Compressor Cascade’” (1992, ASME J. Turbomach., 114, p. 503)

Topics: Boundary layer turbulence, Compressors, Shock waves

Journal Articles

Inlet Flow Angle Determination of Transonic Compressor Cascades

W. Steinert, R. Fuchs, H. Starken

Publisher: ASME

J. Turbomach. July 1992, 114(3): 487–493.

https://doi.org/10.1115/1.2929169

Published Online: July 1, 1992

View Article titled, Inlet Flow Angle Determination of Transonic Compressor Cascades

Topics: Compressors, Flow (Dynamics), Suction, Testing

Journal Articles

Design and Testing of a Controlled Diffusion Airfoil Cascade for Industrial Axial Flow Compressor Application

W. Steinert, B. Eisenberg, H. Starken

Publisher: ASME

J. Turbomach. October 1991, 113(4): 583–590.

https://doi.org/10.1115/1.2929119

Published Online: October 1, 1991

View Article titled, Design and Testing of a Controlled Diffusion Airfoil Cascade for Industrial Axial Flow Compressor Application

Topics: Airfoils, Axial flow, Cascades (Fluid dynamics), Design, Diffusion (Physics), Testing, Compressors, Blades, Boundary layers, Computational methods

Journal Articles

Experimental Investigation of the Performance of a Supersonic Compressor Cascade

D. L. Tweedt, H. A. Schreiber, H. Starken

Publisher: ASME

J. Turbomach. October 1988, 110(4): 456–466.

https://doi.org/10.1115/1.3262219

Published Online: October 1, 1988

View Article titled, Experimental Investigation of the Performance of a Supersonic Compressor Cascade

Topics: Cascades (Fluid dynamics), Compressors, Flow (Dynamics), Mach number, Blades, Pressure, Axial flow, Boundary layers, Density, Design

Journal Articles

Discussion: “Off-Design Performance of Supersonic Compressors With Fixed and Variable Geometry” (Broichhausen, K.-D., Gallus, H. E., and Mo¨nig, R., 1988, ASME J. Turbomach., 110, pp. 312–321)

R. Fuchs, H. Starken

Publisher: ASME

J. Turbomach. July 1988, 110(3): 321–322.

https://doi.org/10.1115/1.3262198

Published Online: July 1, 1988

View Article titled, Discussion: “Off-Design Performance of Supersonic Compressors With Fixed and Variable Geometry” (Broichhausen, K.-D., Gallus, H. E., and Mo¨nig, R., 1988, ASME J. Turbomach., 110, pp. 312–321)

Topics: Compressors, Design, Geometry

Journal citation

NARROW

Supersonic Exit Flow of Two-Dimensional Cascades

Design and Testing of Two Supercritical Compressor Cascades

Supersonic Cascade Interaction

Investigation of the Axial Velocity Density Ratio in a High Turning Cascade

Experimental Investigations of Supersonic Cascades Designed for High Static Pressure Ratios

Redesign and Performance Analysis of a Transonic Axial Compressor Stator and Equivalent Plane Cascades With Subsonic Controlled Diffusion Blades

Experimental Cascade Analysis of a Transonic Compressor Rotor Blade Section

Theoretical and Experimental Analysis of a Compressor Cascade at Supercritical Flow Conditions

Design and Testing of a Controlled Diffusion Airfoil Cascade for Industrial Axial Flow Compressor Application

An Investigation of a Strong Shock-Wave Turbulent Boundary Layer Interaction in a Supersonic Compressor Cascade

Design and Analysis of a High Pitch to Chord Ratio Cascade Representative of Ducted Propfans

Inlet Flow Angle Determination of Transonic Compressor Cascades

Transonic Compressor Rotor Cascade With Boundary-Layer Separation: Experimental and Theoretical Results

Off-Design Transition and Separation Behavior of a CDA Cascade

An Investigation of a Strong Shock-Wave Turbulent Boundary Layer Interaction in a Supersonic Compressor Cascade

Closure to “Discussion of ‘An Investigation of a Strong Shock-Wave Turbulent Boundary Layer Interaction in a Supersonic Compressor Cascade’” (1992, ASME J. Turbomach., 114, p. 503)

Inlet Flow Angle Determination of Transonic Compressor Cascades

Design and Testing of a Controlled Diffusion Airfoil Cascade for Industrial Axial Flow Compressor Application

Experimental Investigation of the Performance of a Supersonic Compressor Cascade

Discussion: “Off-Design Performance of Supersonic Compressors With Fixed and Variable Geometry” (Broichhausen, K.-D., Gallus, H. E., and Mo¨nig, R., 1988, ASME J. Turbomach., 110, pp. 312–321)

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