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Proceedings Papers

Experimental Investigation of an Aggressive S-Shaped Intermediate Compressor Duct

A. Kasper, T. Dygutsch, S. Grund, M. Beversdorff, S. Hakansson, E. Nicke, M. Lejon
Proc. ASME. GT2022, Volume 10C: Turbomachinery — Design Methods and CFD Modeling for Turbomachinery; Ducts, Noise, and Component Interactions, V10CT33A011, June 13–17, 2022
Publisher: American Society of Mechanical Engineers
Paper No: GT2022-82449
https://doi.org/10.1115/GT2022-82449
View Paper titled, Experimental Investigation of an Aggressive S-Shaped Intermediate Compressor Duct
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Topics: Compressors, Ducts, Flow (Dynamics), Inlet guide vanes, Aircraft engines, Blades, Aerospace industry, Aircraft, Airfoils, Annulus
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
Proceedings Papers

A Deep Insight Into the Transonic Flow of an Advanced Centrifugal Compressor Design

D. Wittrock, M. Junker, M. Beversdorff, A. Peters, E. Nicke
Proc. ASME. GT2019, Volume 2B: Turbomachinery, V02BT44A005, June 17–21, 2019
Publisher: American Society of Mechanical Engineers
Paper No: GT2019-90308
https://doi.org/10.1115/GT2019-90308
View Paper titled, A Deep Insight Into the Transonic Flow of an Advanced Centrifugal Compressor Design
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Topics: Compressors, Design, Transonic flow, Inflow, Flow (Dynamics), Impellers, Blades, Lasers, Manufacturing, Numerical analysis
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
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
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

Flow Analysis in a Transonic Centrifugal Compressor Rotor Using 3-Component Laser Velocimetry

H. Krain, G. Karpinski, M. Beversdorff
Proc. ASME. GT2001, Volume 1: Aircraft Engine; Marine; Turbomachinery; Microturbines and Small Turbomachinery, V001T03A019, June 4–7, 2001
Publisher: American Society of Mechanical Engineers
Paper No: 2001-GT-0315
https://doi.org/10.1115/2001-GT-0315
View Paper titled, Flow Analysis in a Transonic Centrifugal Compressor Rotor Using 3-Component Laser Velocimetry
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Topics: Compressors, Flow (Dynamics), Laser velocimetry, Rotors, Optical measurement, Diffusers, High pressure (Physics), Lasers, Machinery, Velocimeters
Proceedings Papers

Improving 3D Flow Characteristics in a Multistage LP Turbine by Means of Endwall Contouring and Airfoil Design Modification: Part 1 — Design and Experimental Investigation

S. Eymann, U. Reinmo¨ller, R. Niehuis, W. Fo¨rster, M. Beversdorff, J. Gier
Proc. ASME. GT2002, Volume 5: Turbo Expo 2002, Parts A and B, 249-260, June 3–6, 2002
Publisher: American Society of Mechanical Engineers
Paper No: GT2002-30352
https://doi.org/10.1115/GT2002-30352
View Paper titled, Improving 3D Flow Characteristics in a Multistage LP Turbine by Means of Endwall Contouring and Airfoil Design Modification: Part 1 — Design and Experimental Investigation
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Topics: Airfoils, Design, Flow (Dynamics), Turbines, Pressure, Aircraft engines, Probes, Circuits, Computer simulation, Lasers