413510
Lehrstuhl und Institut für Strahlantriebe und Turbomaschinen| ID | I:(DE-82)413510_20180101 |
⇦ Lehrstuhl und Institut für Strahlantriebe und Turboarbeitsmaschinen ⇧ RWTH Aachen ⇧
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Dissertation / PhD Thesis
Eine inverse Methode zur Analyse des Wärmeübergangs einer konvektiv gekühlten Gasturbinenschaufel
Aachen : RWTH Aachen University 1 Online-Ressource : Illustrationen (2025) [10.18154/RWTH-2026-04950] = Dissertation, Rheinisch-Westfälische Technische Hochschule Aachen, 2025
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Dissertation / PhD Thesis
Bewertung von Störeinflüssen bei der Messung akustischer Moden in mehrstufigen Axialverdichtern
Aachen : RWTH Aachen University 1 Online-Ressource : Illustrationen (2025) [10.18154/RWTH-2026-03639] = Dissertation, Rheinisch-Westfälische Technische Hochschule Aachen, 2025
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Dissertation / PhD Thesis
Machine learning-enhanced throughflow method for the improved performance prediction of radial impellers
Aachen : RWTH Aachen University 1 Online-Ressource : Illustrationen (2025) [10.18154/RWTH-2026-03280] = Dissertation, Rheinisch-Westfälische Technische Hochschule Aachen, 2025
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Dissertation / PhD Thesis
Analysis of turbulence and loss mechanisms in turbomachinery cascades using high-fidelity simulations
Aachen : RWTH Aachen University 1 Online-Ressource : Illustrationen (2025) [10.18154/RWTH-2026-01454] = Dissertation, Rheinisch-Westfälische Technische Hochschule Aachen, 2025
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Journal Article
Operating Range of Turbocharged Air Supply Systems for Fuel Cell Aircraft Propulsion
Journal of engineering for gas turbines and power 148(1), 011005 (2026) [10.1115/1.4069541]
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Journal Article
Reducing contrail formation by engine design and operating point adaptation of aircraft engines
CEAS Aeronautical Journal 17(2), 913-924 (2025) [10.1007/s13272-025-00887-2]
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Journal Article
Integrated preliminary design of fuel cell propulsion systems for vertical take-off aircraft
CEAS Aeronautical Journal 17(2), 663-676 (2025) [10.1007/s13272-025-00873-8]
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Dissertation / PhD Thesis
Entwurfsmethode für das Thermalmanagement von Brennstoffzellenantrieben in der Luftfahrt
Aachen : RWTH Aachen University 1 Online-Ressource : Illustrationen (2025) [10.18154/RWTH-2025-09848] = Dissertation, Rheinisch-Westfälische Technische Hochschule Aachen, 2025
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Contribution to a book/Contribution to a conference proceedings
Effect of a Sinusoidal Leading Edge Undulation on the Rotor Tip Gap Flow in a Highly Loaded Axial Compressor
Proceedings of ASME Turbo Expo 2025: Turbomachinery Technical Conference and Exposition (GT2025) : June 16-20, 2025, Memphis, Tennessee
ASME Turbo Expo 2025: Turbomachinery Technical Conference and Exposition, Memphis, TNMemphis, TN, USA, 16 Jun 2025 - 20 Jun 2025
Livingston, NJ : American Society of Mechanical Engineers (2025) [10.1115/GT2025-154003]
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Contribution to a book/Contribution to a conference proceedings
Operating Range of Turbocharged Air Supply Systems for PEM Fuel Cell Aircraft Propulsion
Proceedings of ASME Turbo Expo 2025: Turbomachinery Technical Conference and Exposition (GT2025) : June 16-20, 2025, Memphis, Tennessee. - 4
70. ASME Turbomachinery Technical Conference and Exposition, 70. ASME Turbo Expo 2025, Memphis, TNMemphis, TN, USA, 16 Jun 2025 - 20 Jun 2025
Livingston, NJ : American Society of Mechanical Engineers GT2025-151863, V004T06A004, 11 Seiten (2025) [10.1115/GT2025-151863]
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All known publications ...
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