Christoph Jasmund
© Sven Ellger
Christoph Jasmund M.Sc.
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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: 1992
Experiences
- numerical flow simulations
- CAD
- Conducting and evaluating experiments
Current research project
Rotating instabilities in axial compressors
Previous research project
Modification of the cascade wind tunnel for compressor blades with high subsonic flow conditions
Career
| 10/2011-05/2016 | Bachelor's degree in Transport Systems, Technische Universität Berlin Specialization in Aeronautics and Astronautics |
| 10/2015-03/2020 | Master's Degree in Aeronautics and Astronautics, Technische Universität Berlin Priorities: Aerodynamics, Aero Engines |
| 05/2018-06/2018 | Internship WingFan Ltd & Co. KG Activity of the test engineering department at the wind tunnel |
| 06/2018-12/2018 | Internship Lufthansa Technik AG Activity in the field of repair and overhaul of engine parts |
| 01/2019-06/2019 |
Internship Rolls-Royce Deutschland |
| 07/2019-12/2019 | Master's thesis Rolls-Royce Deutschland |
| 03/2020-12/2025 | Research Associate at the Chair of Turbomachinery and Flight Propulsion, TU Dresden |
Publication
2026
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Investigation of Shear Layer Induced Pressure Fluctuations in a Linear Compressor Cascade, May 2026, In: Journal of turbomachinery. 148, 5, 051012Electronic (full-text) versionResearch output: Contribution to journal > Research article
2025
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Investigation of Shear Layer Induced Pressure Fluctuations in a Linear Compressor Cascade, 2025, Proceedings of ASME Turbo Expo 2025: Turbomachinery Technical Conference and Exposition: Turbomachinery: Multidisciplinary Design Approaches, Optimization, and Uncertainty Quantification; Turbomachinery: Radial Turbomachinery Aerodynamics; Turbomachinery: Unsteady Flows in Turbomachinery; Wind Energy; Special Lecture (Invited Only) . American Society of Mechanical Engineers (ASME), Vol. 12. 12 p., GT2025-151156Electronic (full-text) versionResearch output: Contribution to book/conference proceedings/anthology/report > Conference contribution
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The Local Aerodynamic Effect due to Miss-Staggering in Variable Stator Vanes, 2025, ASME Turbo Expo 2025: Turbomachinery Technical Conference and Exposition: Turbomachinery — Axial Flow Fan & Compressor Aerodynamics; Axial Flow Turbine Aerodynamics. American Society of Mechanical Engineers (ASME), Vol. 10. GT2025-151438Electronic (full-text) versionResearch output: Contribution to book/conference proceedings/anthology/report > Conference contribution
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Variation of tip clearance and incidence to induce rotating instabilities in a linear compressor cascade, 2025, Proceedings of the 16th European Conference on Turbomachinery Fluid dynamics & Thermodynamics . ETC2025-137 Electronic (full-text) versionResearch output: Contribution to book/conference proceedings/anthology/report > Conference contribution
2024
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Criteria for the Occurrence of Tip Leakage Flow Induced Rotating Instability, 28 Aug 2024, Turbomachinery - Multidisciplinary Design Approaches, Optimization, and Uncertainty Quantification; Radial Turbomachinery Aerodynamics; Unsteady Flows in Turbomachinery: Turbomachinery Technical Conference and Exposition . Vol. Volume 12D: Turbomachinery — Multidisciplinary Design Approaches, Optimization, and Uncertainty Quantification; Radial Turbom.... 12 p., V12DT36A014Electronic (full-text) versionResearch output: Contribution to book/conference proceedings/anthology/report > Conference contribution
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