Postdoc and Head of Test Lab
Room: 022
Email: martin.bartelt@tu-braunschweig.de
Phone: +49 531 391 9910
Consultation hours: any time on appointment
Working group: Composites
Since 2023 | Postdoc and Head of Test Lab, TU Braunschweig, Institute of Aircraft Design and Lightweight Structures |
2023 | PhD, TU Braunschweig, Institute of Aircraft Design and Lightweight Structures |
2018 - 2023 | Research assistant and PhD student, TU Braunschweig, Institute of Aircraft Design and Lightweight Structures |
2014 - 2018 | Master Aerospace Engineering, TU Braunschweig |
2012 - 2013 | Practical semester WESTFALIA Metal Hoses GmbH, (Shanghai, China und Bristol, USA) |
2010 - 2014 | Bachelor Mechanical Engineering - Manufacturing Technology, Hochschule Aalen |
Research at TU Braunschweig benefits from the broad spectrum of knowledge of over 120 institutes and access to internal structures from professors to first-semester students.
Experimental and numerical optimisation of a hybrid ice protection system and a novel structural design of a thermoplastic slat
Development and construction of a flying demonstrator for active and passive load reduction concepts
Determination of fatigue influences and limits
M. Bartelt: Ermüdungseinflüsse und -grenzen glasfaserverstärkter Kreuzlaminate unter Very High Cycle Fatigue-Belastung, Dissertation, TU Braunschweig – Niedersächsisches Forschungszentrum für Luftfahrt, 2023
M. Bartelt, P. Horst, S. Heimbs: Influence of the stress ratio on the very high cycle fatigue behaviour of composite materials, International Conference on Composite Materials, ICCM23, Belfast, 2023, https://www.iccm-central.org/Proceedings/ICCM23proceedings/papers/ICCM23_Full_Paper_131.pdf
M. Bartelt, P. Horst, S. Heimbs: Effects of an enhanced fibre–matrix adhesion on the fatigue behaviour of composite materials under very high cycle fatigue, CEAS Aeronaut J 14, 753–763 (2023), https://doi.org/10.1007/s13272-023-00673-y
M. Bartelt, T. Luplow, P. Horst, S. Heimbs: Influence of the layer thickness on the very high cycle fatigue behaviour of composite materials, International Committee on Aeronautical Fatigue and Structural Integrity, ICAF, Delft, 2023, https://www.icaf.aero/icaf2023/proceedings/display_manuscript/71.htm
T. Luplow, M. Bartelt, S. Heimbs and P. Horst: Investigation of thickness effects in bi-axially braided glass fibre laminates using a parametrised RVE model, 11th International Conference on Composites Testing and Model Identification, CompTest2023, Girona, 2023, http://hdl.handle.net/10256/23656
F. Runge, S. Starke, L. Markgraf, M. Bartelt, P. Horst, S. Heimbs: Event recognition for realistic load spectra and their impact on inspection intervals in damage-tolerant design, Deutscher Luft- und Raumfahrtkongress, DLRK22, Dresden, 2022, https://doi.org/10.25967/570240
P. Horst, T. J. Adam, M. Lewandrowski, B. Begemann, F. Nolte: Very High Cycle Fatigue – Testing Methods, IOP Conf. Series: Materials Science and Engineering 388, 2018, https://doi.org/10.1088/1757-899X/388/1/012004
International Conference on Very High Cycle Fatigue, VHCF9, Lisbon, Portugal, 2024
Beitrag: Application of a Transverse Crack Initiation Prediction to Four-Point Bending of a Cross-Ply Composite under Very High Cycle Fatigue
European Mechanics of Materials Conference, EMMC19, Madrid, Spain, 2024
Beitrag: Influence of the Loading Type on the Very High Cycle Fatigue Behaviour of Composite Materials
International Conference on Composite Materials, ICCM23, Belfast, Northern Ireland, 2023
Beitrag: Influence of the stress ratio on the very high cycle fatigue behaviour of composite materials
International Committee on Aeronautical Fatigue and Structural Integrity, ICAF, Delft, Netherlands, 2023
Beitrag: Influence of the layer thickness on the very high cycle fatigue behaviour of composite materials (Poster)
Deutscher Luft- und Raumfahrtkongress, DLRK22, Dresden, Deutschland, 2022
Beitrag: Einflüsse einer verbesserten Faser Matrix Adhäsion auf das Ermüdungsverhalten von Verbundmaterialien unter VHCF
Beitrag: Eventerkennung für realistische Lastspektren und deren Einfluss auf Inspektionsintervalle für schadenstolerantes Design