Marcus Wiegand
© Sven Ellger
Wissenschaftlicher Mitarbeiter
NameMr Dipl.-Ing. Marcus Wiegand
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Professur für Turbomaschinen und Flugantriebe
Visiting address:
Zeuner-Bau, Raum 134 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: 1999
Current research project
Engine Performance Modeling of Next Generation Jet Engines – Maple
| 10/2017 - 09/2023 | Dipl.-Ing. in Mechanical Engineering / Aerospace Engineering at TU Dresden, Germany |
| 01/2021 - 01/2022 | Semster abroad at the University of Calgary in Canada and at Chalmers University of Technology in Gothenburg, Sweden |
| 10/2022 - 07/2023 | Internship and diploma thesis at Rolls-Royce Germany |
| since 10/2023 | Research Associate at the Chair of Turbomachinery and Flight Propulsion, TU Dresden, Germany |
Publications
2025
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Robust Design Optimization of a Compressor Rotor Using Recursive Cokriging Based Multi-Fidelity Uncertainty Quantification and Multi-Fidelity Optimization, Jun 2025, In: Journal of Turbomachinery. 147, 6, 12 p., 061009Electronic (full-text) versionResearch output: Contribution to journal > Research article
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Next-Gen Aircraft Engine Design: The Role of Thermo-Fluid Modeling in Performance and Mission-Level Analysis, 3 Jan 2025, AIAA Science and Technology Forum and Exposition, AIAA SciTech Forum 2025. 1715Electronic (full-text) versionResearch output: Contribution to book/conference proceedings/anthology/report > Conference contribution
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Fuel cell hybrid-electric aircraft performance: Optimizing thermal management for reduced climate impact, 2025, Proceedings of ASME Turbo Expo 2025. American Society of Mechanical Engineers (ASME), Vol. 1. GT2025-151328Electronic (full-text) versionResearch output: Contribution to book/conference proceedings/anthology/report > Conference contribution
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Thermofluid Modeling for Next-Generation Aircraft Engine Design, 2025, In: Journal of aircraft. 0, 0, p. 1-11, 11 p.Electronic (full-text) versionResearch output: Contribution to journal > Research article
2024
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Development of a Modular Engine Performance Calculation Tool for Prediction of Conventional and Hybrid-Electric Aircraft Engines, 28 Aug 2024, Aircraft Engine: Turbomachinery Technical Conference and Exposition . Vol. Volume 1: Aircraft Engine. 12 p., V001T01A036Electronic (full-text) versionResearch output: Contribution to book/conference proceedings/anthology/report > Conference contribution
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Robust Design Optimization of a Compressor Rotor Using Recursive Cokriging Based Multi-Fidelity Uncertainty Quantification and Multi-Fidelity Optimization, 28 Aug 2024, Proceedings of the ASME Turbo Expo 2024. The American Society of Mechanical Engineers(ASME), 14 p., GT2024-121977Electronic (full-text) versionResearch output: Contribution to book/conference proceedings/anthology/report > Conference contribution
2023
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Ein modulares Leistungsrechnungsprogramm für konventionelle und hybrid-elektrische Flugantriebe, 27 Oct 2023, 10 p.Electronic (full-text) versionResearch output: Contribution to conferences > Paper
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Entwicklung eines Berechnungsprogramms für disruptive hybrid-elektrische Flugantriebe, 30 May 2023Electronic (full-text) versionResearch output: Contribution to conferences > Poster