From 2002 | Gruppenleiter, Institut für Flugzeugbau und Leichtbau, Technische Universität Braunschweig |
1996 - 2002 | Wissenschaftlicher Assistent, Institut für Flugzeugbau und Leichtbau |
1988 - 1996 | Wissenschaftlicher Mitarbeiter, Institut für Flugzeugbau und Leichtbau |
1996 | Promotion Dr.-Ing., Fakultät Maschinenbau der TU Braunschweig |
1988 | Diplom, Dipl.-Ing. Maschinenbau, TU Braunschwieg |
BionicWalker | Entwicklung einer neuartigen prothetischen Versorgung für teilfußamputierte Patienten mit Carbonfederelement für die Aufnahme, Speicherung und Abgabe von Bewegungsenergie
Hahn, D., Haupt, M., Lobitz, L., Heimbs, S.,. Analysis of the structural behavior of wings with nonlinear components for passive load reduction, 2023. Presented at the Aerospace Europe Conference 2023 (Joint 10th EUCASS & 9th CEAS Conference), Lausanne, Switzerland.
Thel, S., Hahn, D., Haupt, M., Heimbs, S.,. A passive load alleviation aircraft wing: topology optimization for maximizing nonlinear bending–torsion coupling, 2022. Struct Multidisc Optim 65, 155. https://doi.org/10.1007/s00158-022-03248-3
Hahn, D., Haupt, M., Heimbs, S.,. Passive Load Alleviation by Nonlinear Stiffness of Airfoil Structures, 2022, in: AIAA SCITECH 2022 Forum. Presented at the AIAA SCITECH 2022 Forum, American Institute of Aeronautics and Astronautics, San Diego, CA & Virtual. https://doi.org/10.2514/6.2022-0318
Hahn, D., Haupt, M., Exploration of the effect of wing component post-buckling on bending-twist coupling for nonlinear wing twist, 2022. CEAS Aeronaut J. https://doi.org/10.1007/s13272-022-00586-2
Rohdenburg, M., Runge, F., Haupt, M., Markgraf, L., Horst, P., Heimbs, S.:Holistic Low-Effort Model for Damage Tolerance Analysis in Preliminary Design, 2022. Transactions on Aerospace Research 22, 1–20. doi.org/10.2478/tar-2022-0013
Talele, M., Haupt, M., Tooren, M. van, Elham, A.: Concurrent stringer topology and skin steered fiber pattern optimization for grid stiffened composite shell structures, 2021. Composite Structures 266, 113804. https://doi.org/10.1016/j.compstruct.2021.113804
Hötte, F., Sethe, C., Fiedler, T., Haupt, M., Haidn, O.J., Rohdenburg, M.: Experimental Lifetime Study of Regeneratively Cooled Rocket Chamber Walls, 2020. International Journal of Fatigue 105649.
Hötte, F., Haupt, M.C.:Transient 3D conjugate heat transfer simulation of a rectangular GOX–GCH4 rocket combustion chamber and validation, 2020. Aerospace Science and Technology 105, 106043.
Hötte, F.; Lungu, P.; von Sethe, C.; Fiedler, T.; Haupt, M.C.; Haidn, O.J.: Experimental Investigations of Thermomechanical Fluid-Structure Interaction in Rocket Combustion Chambers, AIAA Journal of Propulsion and Power, 35(5):906-916, 2019
Sommerwerk, K.; Michels, B.; Haupt, M.C.; Horst, P.: Influence of engine modeling on structural sizing and approach aerodynamics of a circulation controlled wing. CEAS Aeronautical Journal, 9(1):219-233, 2018
Sommerwerk, K.; Woidt, M.; Haupt, M.; Horst, P.: Reissner–Mindlin shell implementation and energy conserving isogeometric multi-patch coupling; International Journal for Numerical Methods in Engineering, 109(7):982–1012, 2017
Haupt, M.; Kowollik, D.; Lindhorst, K.; Hötte, F.: Fluid-Structure-Interaction in Rocket Thrust Chambers Simulation and Validation. Defect and Diffusion Forum, 366:97-117, 2016
Lindhorst, K.; Haupt, M.; Horst, P.: Reduced-order modelling of non-linear, transient aero-dynamics of the HIRENASD wing; Aeronautical Journal, 120(1226):601-626, 2016.
Lindhorst, K.; Haupt, M.C.; Horst, P.: Aeroelastic Analyses of the High-Reynolds-Number-Aerostructural-Dynamics Configuration Using a Nonlinear Surrogate Model Approach. AIAA Journal, 53(9):2784-2796, 2015
Lindhorst, K.; Haupt, M.C.; Horst, P.: Efficient Surrogate Modelling of Nonlinear Aerodynamics in Aerostructural Coupling Schemes. AIAA Journal, 52:1952-1966, 2014
Sommerwerk, K.; Haupt, M. C.: Design analysis and sizing of a circulation controlled CFRP wing with Coanda flaps via CFD-CSM coupling. CEAS Aeronautical Journal, 5(1):95-108, 2014
Kowollik, D.; Tini, V.; Reese, S.; Haupt, M.C.: 3D fluid-structure interaction analysis of a typical liquid rocket engine based on a novel viscoplastic damage model. International Journal for Numerical Methods in Engineering, 94:1165-1190, 2013
Möhle, E.; Haupt, M.C.; Horst, P.: Coupled Numerical Simulation and Experimental Validation of the Electro Impulse De-Icing Process. J. of Aircraft, 50:96-102, 2013
Unger, R.; Haupt, M.C.; Horst P.; Radespiel R.: Fluid-structure analysis of a flexible flapping airfoil at low Reynolds number flow. J. of Fluids and Structures, 28:72-88, 2012