Björn Koppe
© Michael Kretzschmar
Dipl.-Ing. Björn Koppe
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Professur für Turbomaschinen und Flugantriebe
Visiting address:
Zeuner-Bau, ZEU 156 George-Bähr-Strasse 3c
01069 Dresden
Postal address:
TUD Dresden University of Technology
Institut für Strömungsmechanik
Professur für Turbomaschinen und Flugantriebe
01062 Dresden
Curriculum vitae
Year of birth : 1990
Knowledge
- numercal flow simulation
- programming
Current research projects
Periodic unsteady flow near the endwall in rotating annular compressor cascades
Career
| 10/2011 – 08/2017 | Study of Mechanical Engineering/Aerospace at TU Dresden |
| 10/2013 – 08/2014 | Student assistant at the Institute of Fluid Mechanics, TU Dresden |
| 12/2014 – 04/2015 | Internship at Rolls-Royce Deutschland |
| 01/2017 – 07/2017 | Dipl.-Ing. thesis at Rolls-Royce Deutschland |
| 02/2018 - 06/2024 | Research Associate at the Chair of Turbomachinery and Flight Propulsion, Technische Universität Dresden |
Publications
Chen, X., Lange, M., Koppe, B., Jasmund, C., Chu, W., Mailach, R.:
"Criteria for the Occurrence of Tip Leakage Flow Induced Rotating Instability “
ASME TURBO Expo 2024, London, GT2024-126921.
Koppe, B., Lange, M., Mailach, R.
„Effect of Incoming Wakes on the Passage Flow of an Axial Compressor Rotor”
ASME Turbo Expo 2023, GT2023-102268, Boston, USA, 2023
Chen, X., Koppe, B., Lange, M., Chu, W., Mailach, R.:
"Comparison of Turbulence Modeling for a Compressor Rotor at Different Tip Clearances"
AIAA Journal 2022, 60:2, 1186 – 1198: https://doi.org/10.2514/1.J060468
Chen, X., Koppe, B., Lange, M., Chu, W., Mailach, R.:
"Rotating Instabilities in a Low-Speed Single Compressor Rotor Row with Varying Blade Tip Clearance" Energies, 2021, 14(24), 8369
https://doi.org/10.3390/en14248369
Koppe, B., Lange, M., Mailach, R.:
"Influence of Boundary Layer Skew on the Tip Leakage Vortex of an Axial Compressor Stator", ASME J. Turbomach. September 2021, 143(9): 091016
https://doi.org/10.1115/1.4050628
Ventosa-Molina, J., Koppe, B., Lange, M., Mailach, R., Fröhlich, J.
"Effects of Rotation on the Flow Structure in a Compressor Cascade"
ASME Turbo Expo 2021, GT2021-58793, virtual conference, 2021
ASME. J. Turbomach. August 2022; 144(8): 081006
https://doi.org/10.1115/1.4053537
Chen, X., Koppe, B., Lange, M., Chu, W., Mailach, R.
"Performance of Unsteady Reynolds-Averaged Navier-Stokes and Hybrid Scale-Resolving Simulation Approaches in Simulating a Low-Speed Axial Compressor Single Rotor"
ASME Turbo Expo 2021, GT2021-59028, virtual conference, 2021
https://doi.org/10.1115/GT2021-59028
Engelmann D, Sinkwitz M, di Mare F, Koppe B, Mailach R, Ventosa-Molina J, Fröhlich J, Schubert T, Niehuis R.
"Near-Wall Flow in Turbomachinery Cascades - Results of a German Collaborative Project" International Journal of Turbomachinery, Propulsion and Power, 2021; 6(2):9 https://doi.org/10.3390/ijtpp6020009
Koppe, B., Lange, M., Mailach, R.
"Influence of Boundary Layer Skew on the Tip Leakage Vortex of an Axial Compressor Stator"
ASME Turbo Expo 2020, GT2020-15940, virtual conference, 2020
https://doi.org/10.1115/GT2020-15940