Chen Xiangyi
Xiangyi Chen M.Eng
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Professur für Turbomaschinen und Flugantriebe
Visiting address:
Zeuner-Bau, Raum 156 George-Bähr-Strasse 3c
01069 Dresden
Curriculum vitae
Year of birth: 1993
Experiences
- Computational Fluid Dynamics
- fluid mechanics
- flow control in turbomachinery
Current research project
Career
09/2011-06/2015 | Bachelor in Flight Vehicle Propulsion Engineering at Northwestern Polytechnical University |
09/2015-08/2017 | Master in Aerospace Propulsion Theory and Engineering at Northwestern Polytechnical University |
09/2017-10/2019 | Research associate at Northwestern Polytechnical University |
since 11/2019 | Research Associate at the Chair of Turbomachinery and Flight Propulsion, Technische Universität Dresden Scholarship by CSC |
Publications
Xiangyi Chen
Numerical investigation of rotating instabilities in axial compressors
(Dissertation, Technische Universität Dresden, 2022)
published at TUDpress 2023, Band 38 der Schriftenreihe aus dem Institut für Strömungsmechanik, Dresden, ISBN: 978-3-95908-307-2
Chen, X., Koppe, B., Lange, M., Chu, W., Mailach, R.:
"Influence of Casing Groove on Rotating Instabilities in a Low-Speed Axial Compressor"
ASME J. Turbomach. July 2023, 145(7): 071015 https://doi.org/10.1115/1.4056863
Chen, X., Koppe, B., Lange, M., Chu, W., Mailach, R.:
"Influence of Casing Groove on Rotating Instabilities in a Low-Speed Axial Compressor"
ASME Turbo Expo 2022, GT2022-82101, Rotterdam, 2022
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
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.
Chen, X., Chu, W., Zhang, H., Li, X. Numerical study on inlet angle of guide vane in recess vaned casing treatment. Aerospace Science and Technology, 93, 105323, 2019.
Chen, X., Chu, W., Zhang, H., Luo, B., 2019. Numerical Investigation of Cut-corner in the Recess Vaned Casing Treatment. ASME Turbo Expo, GT2019-90751, 2019.
Chen, X., Chu, W., Zhang, H., Li, J., Lang, J., 2017. Numerical Investigation of Effect of Recess Vane Casing Treatments on an Axial Lift Fan Performance. ASME Turbo Expo, GT2017-63767, 2017.