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Proceedings Papers

Insights Into the Unsteady Shock Boundary Layer Interaction

A. Hergt, J. Klinner, C. Willert, S. Grund, W. Steinert
Proc. ASME. GT2022, Volume 10A: Turbomachinery — Axial Flow Fan and Compressor Aerodynamics, V10AT29A033, June 13–17, 2022
Publisher: American Society of Mechanical Engineers
Paper No: GT2022-82720
https://doi.org/10.1115/GT2022-82720
View Paper titled, Insights Into the Unsteady Shock Boundary Layer Interaction
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Topics: Boundary layers, Shock (Mechanics), Oscillations, Blades, Flow (Dynamics), Cascades (Fluid dynamics), Compressors, Inflow, Vibration, Mach number
Journal Articles

On the Importance of Transition Control at Transonic Compressor Blades

Alexander Hergt, J. Klinner, S. Grund, C. Willert, W. Steinert, M. Beversdorff
Journal: Journal of Turbomachinery
Publisher: ASME
Article Type: Research Papers
J. Turbomach. March 2021, 143(3): 031007.
Paper No: TURBO-20-1102
https://doi.org/10.1115/1.4049783
Published Online: March 1, 2021
View Article titled, On the Importance of Transition Control at Transonic Compressor Blades
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Topics: Blades, Boundary layers, Cascades (Fluid dynamics), Compressors, Oscillations, Shock (Mechanics), Flow (Dynamics), Separation (Technology), Suction, Flow control
Proceedings Papers

On the Importance of Transition Control at Transonic Compressor Blades

A. Hergt, J. Klinner, S. Grund, C. Willert, W. Steinert, M. Beversdorff
Proc. ASME. GT2019, Volume 2A: Turbomachinery, V02AT39A009, June 17–21, 2019
Publisher: American Society of Mechanical Engineers
Paper No: GT2019-90440
https://doi.org/10.1115/GT2019-90440
View Paper titled, On the Importance of Transition Control at Transonic Compressor Blades
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Topics: Blades, Compressors, Shock waves, Cascades (Fluid dynamics), Flow (Dynamics), Oscillations, Boundary layers, Shock (Mechanics), Air jets, Boundary layer turbulence
Journal Articles

Some Aspects of the Transonic Compressor Tandem Design

Alexander Hergt, S. Grund, J. Klinner, W. Steinert, M. Beversdorff, U. Siller
Journal: Journal of Turbomachinery
Publisher: ASME
Article Type: Research-Article
J. Turbomach. September 2019, 141(9): 091003.
Paper No: TURBO-18-1243
https://doi.org/10.1115/1.4043280
Published Online: May 30, 2019
View Article titled, Some Aspects of the Transonic Compressor Tandem Design
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Topics: Blades, Cascades (Fluid dynamics), Compressors, Design, Optimization, Flow (Dynamics), Mach number, Wakes
Journal Articles

The Present Challenge of Transonic Compressor Blade Design

Alexander Hergt, J. Klinner, J. Wellner, C. Willert, S. Grund, W. Steinert, M. Beversdorff
Journal: Journal of Turbomachinery
Publisher: ASME
Article Type: Research-Article
J. Turbomach. September 2019, 141(9): 091004.
Paper No: TURBO-18-1244
https://doi.org/10.1115/1.4043329
Published Online: May 30, 2019
View Article titled, The Present Challenge of Transonic Compressor Blade Design
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Topics: Blades, Boundary layers, Cascades (Fluid dynamics), Compressors, Design, Flow (Dynamics), Shock (Mechanics), Shock waves, Turbulence, Suction
Proceedings Papers

Some Aspects of Transonic Compressor Tandem Design

A. Hergt, S. Grund, J. Klinner, W. Steinert, M. Beversdorff, U. Siller
Proc. ASME. GT2018, Volume 2A: Turbomachinery, V02AT39A004, June 11–15, 2018
Publisher: American Society of Mechanical Engineers
Paper No: GT2018-75132
https://doi.org/10.1115/GT2018-75132
View Paper titled, Some Aspects of Transonic Compressor Tandem Design
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Topics: Compressors, Design, Cascades (Fluid dynamics), Blades, Wakes, Deflection, Inflow, Mach number, Computer simulation, Construction
Proceedings Papers

The Present Challenge of Transonic Compressor Blade Design

A. Hergt, J. Klinner, J. Wellner, C. Willert, S. Grund, W. Steinert, M. Beversdorff
Proc. ASME. GT2018, Volume 2A: Turbomachinery, V02AT39A012, June 11–15, 2018
Publisher: American Society of Mechanical Engineers
Paper No: GT2018-75528
https://doi.org/10.1115/GT2018-75528
View Paper titled, The Present Challenge of Transonic Compressor Blade Design
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Topics: Blades, Compressors, Design, Cascades (Fluid dynamics), Flow (Dynamics), Shock waves, Simulation, Boundary layers, Inflow, Unsteady flow
Journal Articles

Riblet Application in Compressors: Toward Efficient Blade Design

Alexander Hergt, W. Hage, S. Grund, W. Steinert, M. Terhorst, F. Schongen, Y. Wilke
Journal: Journal of Turbomachinery
Publisher: ASME
Article Type: Research-Article
J. Turbomach. November 2015, 137(11): 111006.
Paper No: TURBO-15-1103
https://doi.org/10.1115/1.4031090
Published Online: September 16, 2015
View Article titled, Riblet Application in Compressors: Toward Efficient Blade Design
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Topics: Blades, Cascades (Fluid dynamics), Compressors, Design, Optimization, Reynolds number, Manufacturing, Pressure, Flow (Dynamics)
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
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Topics: Airfoils, Axial flow, Cascades (Fluid dynamics), Design, Diffusion (Physics), Testing, Compressors, Blades, Boundary layers, Computational methods
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
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Topics: Compressors, Flow (Dynamics), Mach number, Suction, Testing
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
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Topics: Cascades (Fluid dynamics), Chords (Trusses), Design, Blades, Mach number, Boundary layers, Pressure, Aircraft engines, Flow (Dynamics), Flow turning
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
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Topics: Boundary layers, Cascades (Fluid dynamics), Compressors, Rotors, Separation (Technology), Design, Mach number, Bubbles, Flow (Dynamics), Blades
Proceedings Papers

The Effect of an Eroded Leading Edge on the Aerodynamic Performance of a Transonic Fan Blade Cascade

A. Hergt, J. Klinner, W. Steinert, S. Grund, M. Beversdorff, A. Giebmanns, R. Schnell
Proc. ASME. GT2014, Volume 2A: Turbomachinery, V02AT37A001, June 16–20, 2014
Publisher: American Society of Mechanical Engineers
Paper No: GT2014-25023
https://doi.org/10.1115/GT2014-25023
View Paper titled, The Effect of an Eroded Leading Edge on the Aerodynamic Performance of a Transonic Fan Blade Cascade
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Topics: Blades, Cascades (Fluid dynamics), Shock (Mechanics), Shapes, Chords (Trusses), Erosion, Inflow, Suction, Boundary layers, Bubbles
Proceedings Papers

Riblet Application in Compressors: Towards Efficient Blade Design?

A. Hergt, W. Hage, S. Grund, W. Steinert, M. Terhorst, F. Schongen, Y. Wilke
Proc. ASME. GT2014, Volume 2A: Turbomachinery, V02AT37A006, June 16–20, 2014
Publisher: American Society of Mechanical Engineers
Paper No: GT2014-25142
https://doi.org/10.1115/GT2014-25142
View Paper titled, Riblet Application in Compressors: Towards Efficient Blade Design?
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Topics: Blades, Compressors, Design, Cascades (Fluid dynamics), Reynolds number, Manufacturing, Optimization, Suction, Turbulence, Coating processes
Journal Articles

The Effect of an Eroded Leading Edge on the Aerodynamic Performance of a Transonic Fan Blade Cascade

Alexander Hergt, J. Klinner, W. Steinert, S. Grund, M. Beversdorff, A. Giebmanns, R. Schnell
Journal: Journal of Turbomachinery
Publisher: ASME
Article Type: Research-Article
J. Turbomach. February 2015, 137(2): 021006.
Paper No: TURBO-14-1112
https://doi.org/10.1115/1.4028215
Published Online: September 16, 2014
View Article titled, The Effect of an Eroded Leading Edge on the Aerodynamic Performance of a Transonic Fan Blade Cascade
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Topics: Blades, Cascades (Fluid dynamics), Shock (Mechanics), Suction
Proceedings Papers

Analyzing and Optimizing Geometrically Degraded Transonic Fan Blades by Means of 2D and 3D Simulations and Cascade Measurements

A. Giebmanns, R. Schnell, W. Steinert, A. Hergt, E. Nicke, C. Werner-Spatz
Proc. ASME. GT2012, Volume 8: Turbomachinery, Parts A, B, and C, 279-288, June 11–15, 2012
Publisher: American Society of Mechanical Engineers
Paper No: GT2012-69064
https://doi.org/10.1115/GT2012-69064
View Paper titled, Analyzing and Optimizing Geometrically Degraded Transonic Fan Blades by Means of 2D and 3D Simulations and Cascade Measurements
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Topics: Blades, Cascades (Fluid dynamics), Engineering simulation, Simulation, Engines, Airfoils, Chords (Trusses), Erosion, Liquid crystals, Optimization
Journal Articles

Off-Design Transition and Separation Behavior of a CDA Cascade

W. Steinert, H. Starken
Journal: Journal of Turbomachinery
Publisher: ASME
Article Type: Research Papers
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
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Topics: Cascades (Fluid dynamics), Design, Separation (Technology), Blades, Airfoils, Axial flow, Boundary layers, Compressors, Diffusion (Physics), Inks
Journal Articles

Inlet Flow Angle Determination of Transonic Compressor Cascades

W. Steinert, R. Fuchs, H. Starken
Journal: Journal of Turbomachinery
Publisher: ASME
Article Type: Research Papers
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
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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
Journal: Journal of Turbomachinery
Publisher: ASME
Article Type: Research Papers
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
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Topics: Airfoils, Axial flow, Cascades (Fluid dynamics), Design, Diffusion (Physics), Testing, Compressors, Blades, Boundary layers, Computational methods
Journal Articles

Comparison of Controlled Diffusion Airfoils With Conventional NACA 65 Airfoils Developed for Stator Blade Application in a Multistage Axial Compressor

H. Rechter, W. Steinert, K. Lehmann
Journal: Journal of Engineering for Gas Turbines and Power
Publisher: ASME
Article Type: Research Papers
J. Eng. Gas Turbines Power. April 1985, 107(2): 494–498.
https://doi.org/10.1115/1.3239758
Published Online: April 1, 1985
View Article titled, Comparison of Controlled Diffusion Airfoils With Conventional NACA 65 Airfoils Developed for Stator Blade Application in a Multistage Axial Compressor
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Topics: Airfoils, Blades, Compressors, Diffusion (Physics), Stators, Cascades (Fluid dynamics), Design, Test facilities, Turning angles, Wind tunnels