Bücher, Monographien
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(2020): Experimental Validation of an Optimized Design Process for Transonic Mixed-Flow Compressors, Contributions to the Final Symposium of the Collaborative Research Center 880, December 17-18, 2019, Braunschweig, Germany
DOI: 10.1007/978-3-030-52429-6
ISBN: 978-3-030-52428-9
Dissertationen
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(2023): Aeroelastische Auswirkungen der Schaufel-Rotor-Interaktionin einem 1 1/2-stufigen Axialverdichter, Hannover: Gottfried Wilhelm Leibniz Universität, Diss., 2023, Band 34, xee, 143 S.
DOI: 10.15488/15543
Internationale Konferenzbeiträge, begutachtet
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(2024): Aeroelastic Influence of Blade-Shaft Coupling in a 1 1.5-Stage Axial Compressor, ASME Turbo Expo 2024: Turbomachinery Technical Conference and Exposition
DOI: 10.1115/GT2024-124275
ISSN: GT2024-124275 -
(2023): Characterizing the Unsteady Flow Field in Low-Flow Turbine Operation, Turbo Expo: Power for Land, Sea, and Air, vol. 87110, p. V13DT36A018. American Society of Mechanical Engineers
DOI: 10.1115/GT2023-102813 -
(2022): An Improved Reduced Order Model for Bladed Disks Including Multistage Aeroelastic and Structural Coupling, Proceedings of Global Power and Propulsion Society. ISSN-Nr: 2504-4400. GPPS Chania22
DOI: 10.33737/gpps22-tc-106 -
(2020): Design of a Mixed-Flow Transonic Compressor for Active High-Lift System Using a 3D Inverse Design Methodology, Proceedings of ASME Turbo Expo 2020 Turbomachinery Technical Conference and Exposition GT2020, September 21-25, 2020, Virtual, Online, GT2020-15645
DOI: 10.1115/GT2020-15645
ISBN: 978-0-7918-8410-2 -
(2019): Experimental Validation of a Compact Mixed-Flow Compressor for an Active High-Lift System, IOP Conference Series: Materials Science and Engineering: Volume 643, Number 1
DOI: 10.1088/1757-899X/643/1/012142
Internationale wissenschaftliche Beiträge in Fachzeitschriften, begutachtet
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(2024): Modal Parameter Estimation of Turbomachinery in Operation Taking into Account Friction Damping, Mechanical Systems and Signal Processing, Vol. 216, Page 111414
DOI: 10.1016/j.ymssp.2024.111414 -
(2024): Characterizing the Unsteady Flow Field in Low-Flow Turbine Operation, Journal of Turbomachinery, Volume 146, Number 10
DOI: 10.1115/1.4065243 -
(2024): Aeroelastic Influence of Blade-Shaft Coupling in a 1 1.5-Stage Axial Compressor, Journal of Engineering for Gas Turbines and Power
DOI: 10.1115/1.4066372 -
(2023): An Improved Reduced Order Model for Bladed Disks Including Multistage Aeroelastic and Structural Coupling, Journal of the Global Power and Propulsion Society, Vol. 7, S. 140-152
DOI: 10.33737/jgpps/161707 -
(2023): Multidisciplinary Design of an Electrically Powered High-Lift System, ASME Journal of Turbomachinery, Vol. 145
DOI: 10.1115/1.4062677 -
(2022): Forced Response Due to Vane Stagger Angle Variation in an Axial Compressor, ASME. J. Turbomach. August 2022; 144(8): 081011
DOI: 10.1115/1.4053839 -
(2022): Reduced Order Modeling of Forced Response in a Multistage Compressor Under Mistuning and Aerocoupling, Journal of Engineering for Gas Turbines and Power
DOI: 10.1115/1.4055368
Nationale Konferenzbeiträge, nicht begutachtet
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(2020): Investigation of Multiharmonic Effects in a Single Stage High Speed Compressor, Deutscher Luft- und Raumfahrtkongress 2019, Darmstadt, Deutsche Gesellschaft für Luft- und Raumfahrt
DOI: 10.25967/490212
Veröffentlichte Berichte
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(2022): Stall Behaviour in a Mixed-flow Compressor with Axial Slot Casing Treatment, Journal of Thermal Science 31, 13-24